Computational fluid dynamics
Resource Information
The concept Computational fluid dynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri Libraries.
The Resource
Computational fluid dynamics
Resource Information
The concept Computational fluid dynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri Libraries.
- Label
- Computational fluid dynamics
- Source
- nasat
686 Items that share the Concept Computational fluid dynamics
Context
Context of Computational fluid dynamicsSubject of
No resources found
No enriched resources found
- [Analysis and development of finite element methods for the study of nonlinear thermomechanical behavior of structural components]
- 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Los Angeles, California, February 9-13, 1998
- 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999
- A CFD analysis of hydrogen leakage during on-pad purge in the ORION/ARES I shared volume
- A CFD study of tilt rotor flowfields
- A CFD-based study of the feasibility of adapting an erosion burner rig for examining the effect of CMAS deposition/corrosion on environmental barrier coatings
- A CFD/CSD interaction methodology for aircraft wings : a dissertation ...
- A comparison of interactional aerodynamics methods for a helicopter in low speed flight
- A comparison of lifting-line and CFD methods with flight test data from a research puma helicopter
- A computational examination of directional stability for smooth and chined forebodies at High-Ü
- A computational fluid dynamic and heat transfer model for gaseous core and gas cooled space power and propulsion reactors
- A computational investigation of gear windage
- A computational methodology for simulating thermal loss testing of the Advanced Stirling C
- A computational study of multiple jet and wall interaction
- A cost-effective strategy for nonoscillatory convection without clipping
- A critical comparison of turbulence models for homogeneous shear flows in a rotating frame
- A dual potential formulation of the Navier-Stokes equations
- A dual-plane PIV study of turbulent heat transfer flows
- A fast parallel tridiagonal algorithm for a class of CFD applications
- A generalized fluid system simulation program to model flow distribution in fluid networks : draft paper ...
- A generalized wall function
- A genuninely multi-dimensional upwind cell-vertex scheme for the Euler equations
- A high order discontinuous Galerkin method for 2D incompressible flows
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A hybrid numerical method for turbulent mixing layers
- A knowledge-based approach to automated flow-field zoning for computational fluid dynamics
- A least-squares finite element method for electromagnetic scattering problems
- A method for generating reduced order linear models of supersonic inlets : under grant NAG3-1450
- A method for generating reduced-order linear models of multidimensional supersonic inlets
- A modeling technique for STOVL ejector and volume dynamics
- A non-cut cell immersed boundary method for use in icing simulations
- A novel potential viscous flow coupling technique for computing helicopter flow fields
- A novel shape parameterization approach
- A numerical analysis of heat transfer and effectiveness on film cooled turbine blade tip models
- A numerical and experimental analysis of reactor performance and deposition rates for CVD on monofilaments
- A numerical method for incompressible flow with heat transfer
- A numerical turbulence model for multiphase flows in the protoplanetary nebula
- A preconditioning method for shape optimization governed by the Euler equations
- A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers
- A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
- A semantic analysis method for scientific and engineering code
- A simplified self-adaptive grid method, SAGE
- A study of pump cavitation damage
- A three-dimensional CFD investigation of secondary flow in an accelerating, 90 eÌŠlbow
- A three-dimensional unsteady CFD model of compressor stability
- A user's guide to CGNS
- A user's manual for ROTTILT solver : tiltrotor fountain flow field prediction
- ADPAC v1.0 : user's manual
- Accuracy of schemes for the Euler equations with non-uniform meshes
- Accuracy of schemes with nonuniform meshes for compressible fluid flows
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Active control of flow separation over an airfoil
- Adaptive meshing techniques for viscous flow calculations on mixed element unstructured meshes
- Advanced low-noise research fan stage design
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Aero-heating of shallow cavities in hypersonic freestream flow
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations
- Aerodynamic design and computational analysis of a spacecraft cabin ventilation fan
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Aerodynamic flow field measurements for automotive systems
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aeroelastic analysis of aircraft : wing and wing/fuselage configurations
- Aeroelastic calculations using CFD for a typical business jet model
- Aeroelastic computations of a compressor stage using the harmonic balance method
- Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications : final report for the period December 1, 1995 through Novemeber 30, 1996
- Aeromechanics analysis of a boundary layer ingesting fan
- Aeropropulsion technology (APT) : task 23--stator seal cavity flow investigation
- Algebraic turbulence modeling for unstructured and adaptive meshes
- An LU implicit scheme for high speed inlet analysis
- An NPARC turbulence module with wall functions : under cooperative agreement NCC3-370
- An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations : annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760
- An application of the difference potentials method to solving external problems in CFD
- An application of the difference potentials method to solving external problems in CFD
- An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization
- An efficient multiblock method for aerodynamic analysis and design on distributed memory systems : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997
- An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers
- An experimental and numerical investigation of turbulent vortex breakdown and aircraft wakes : final report, contract NAG 1-1775
- An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft
- An experimental approach to a rapid propulsion and aeronautics concepts testbed
- An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel
- An experimental study of the Ground Transportation System (GTS) model in the NASA Ames 7-by-10-Ft Wind Tunnel
- An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, July 1, 1987-December 31, 1987
- An inviscid computational study of an X-33 configuration at hypersonic speeds
- An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- An upwind-differencing scheme for the incompressible Navier-Stokes equations
- Analysis of a hovering rotor in icing conditions
- Analysis of a rocket based combined cycle engine during rocket only operation
- Analysis of buzz in a supersonic inlet
- Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of internal flows relative to the space shuttle main engine : final report
- Analysis of lean premixed/prevaporized combustion with KIVA-II
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Analysis of the STS-126 flow control valve structural-acoustic coupling failure
- Analytical study of the origin and behavior of asymmetric vortices
- Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of a high-fidelity icing analysis method to a model-scale rotor in forward flight
- Application of computational fluid dynamics in high speed aeropropulsion
- Application of low dimensional manifolds in NOx prediction : under cooperative agreement NCC3-534
- Applications of the Lattice Boltzmann method to complex and turbulent flows
- Ares I Scale Model Acoustic Test overpressure results
- Artificial boundary conditions based on the difference potentials method
- Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods
- Assessment of NASA's aircraft noise prediction capability
- Assessment of an explicit algebraic Reynolds stress model
- Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction
- Assessment of some atomization models used in spray calculations
- Atomization simulations using an Eulerian-VOF-Lagrangian method
- Automated boundary conditions for wind tunnel simulations
- Axial and centrifugal compressor mean line flow analysis method
- Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition, part 1, Computational fluid dynamics (CFD) investigation
- Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel
- Beta testing of CFD code for the analysis of combustion systems
- Bidirectional brush seals : post-test analysis
- Bidirectional brush seals--post-test analysis
- Blended wing body concept development with open rotor engine integration
- Burner rig with an unattached duct for evaluating the erosion resistance of thermal barrier coatings
- CFD analysis and design optimization using parallel computers
- CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility
- CFD analysis of nozzle jet plume effects on sonic boom signature
- CFD for hypersonic propulsion
- CFD modeling of free-piston Stirling engines
- CFD modelling of bore erosion in two-stage light gas guns
- CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report
- CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system : final report : under contract NAG3-1500
- CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction
- CFL3D contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
- CFL3D user's manual (version 5.0)
- CFL3D, its history and some recent applications
- CMOTT turbulence module for NPARC : under cooperative agreement NCC3-520
- Calculation of multistage turbomachinery using steady characteristic boundary conditions
- Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Calculations of diffuser flows with an anisotropic K-[epsilon] model
- Capillary channel flow (CCF) EU2-02 on the International Space Station (ISS) : an experimental investigation of passive bubble separations in an open capillary channel
- Cause and cure : deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids
- Combined experimental and numerical simulations of thermal barrier coated turbine blades erosion
- Comments on the diffusive behavior of two upwind schemes
- Comments on the diffusive behavior of two upwind schemes
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparative study of advanced turbulence models for turbomachinery : contract NAS8-38860, final report
- Comparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow
- Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
- Comparison of NACA 0012 laminar flow solutions : structured and unstructured grid methods
- Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer
- Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine
- Comparison of several numerical methods for simulation of compressible shear layers
- Comparison of the booster interface temperature in stainless steel (SS) v-channel versus the aluminum (Al) y-channel Primer Chamber Assemblies (PCAs)
- Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin
- Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating
- Compliant turbomachine sealing
- Compressibility considerations for [kappa-omega] turbulence models in hypersonic boundary layer applications
- Compressible flows with periodic vortical disturbances around lifting airfoils
- Computation of Navier-Stokes equations for three-dimensional flow separation
- Computation of lifting wing-flap configurations : NASA grant NCC2-5070, final report ... funding dates: July 1, 1994 to June 30, 1995
- Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
- Computation of separated and unsteady flows with one- and two-equation turbulence models : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of viscous flow in curved ducts and comparison with experimental data
- Computation of viscous incompressible flows
- Computational Fluid Dynamics (CFD) analysis for the reduction of impeller discharge flow distortion
- Computational Fluid Dynamics (CFD) simulations of jet mixing in tanks of different scales
- Computational aeroacoustics and numerical simulation of supersonic jets : final report on NASA grant NAG 1-1479
- Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development
- Computational aerodynamic simulations of a spacecraft cabin ventilation fan design
- Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development
- Computational aeroheating predictions for X-34
- Computational aeroheating predictions for X-34
- Computational aeroservoelastic analysis with an Euler-based unsteady flow solver : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997
- Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff
- Computational analysis of a low-boom supersonic inlet
- Computational analysis of the SSME fuel preburner flow : final report
- Computational analysis of the combustion process in an axisymmetric RBCC flowpath
- Computational analysis of the combustion process in an axisymmetric,RBCC flowpath
- Computational assessment of the aerodynamic performance of a variable-speed power turbine for large civil tilt-rotor application
- Computational fluid mechanics utilizing the variational principle of modeling damping seals
- Computational icing risk analysis of the D8 "Double Bubble" aircraft
- Computational investigation of flap-edges : final report, NASA award NCC-2-857
- Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades
- Computational investigation of tangential slot blowing on a generic chined forebody
- Computational modeling and validation for hypersonic inlets
- Computational pollutant environment assessment from propulsion-system testing
- Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of separating flow in a planar subsonic diffuser
- Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
- Computational study of the CC3 impeller and vaneless diffuser experiment
- Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
- Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
- Computational work to support FAP/SRW variable-speed power-turbine development
- Computational/experimental aeroheating predictions for X-33 phase II vehicle
- Computations of axisymmetric flows in hypersonic shock tubes
- Computations of complex three-dimensional turbulent free jets
- Computer Aided Grid Interface : an interactive CFD pre-processor, final report, (performance period--16 May 1991-15 May 1996)
- Computer simulation of aircraft aerodynamics
- Concept evaluation : NASA reference model 2--side by side
- Conjugate heat transfer analyses on the manifold for ramjet fuel injectors
- Connection between the lattice Boltzmann equation and the beam scheme
- Conservational PDF equations of turbulence
- Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers
- Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations
- Convergence analysis of turbulent flow solutions
- Correlation of Puma airloads : lifting-line and wake calculation
- Correlation of puma airloads : evaluation of CFD prediction methods
- Critical assessment of Reynolds stress turbulence models using homogeneous flows
- Cryogenic fluid storage technology development : recent and planned efforts at NASA
- Current capabilities and future directions in computational fluid dynamics
- Current status of post-combustor trace chemistry modeling and simulation at NASA Glenn Research Center
- Current status of superheat spray modeling with NCC
- Data Parallel Line Relaxation (DPLR) code user manual : Acadia version 4.01.1
- Data driven model development for the supersonic semispan transport (S4T)
- Design and analysis of an isokinetic sampling probe for submicron particle measurements at high altitude
- Design and analysis tool for external-compression supersonic inlets
- Detailed experimental data for CFD code validation
- Deterministic stress modeling of hot gas segregation in a turbine
- Development and demonstration of a computational tool for the analysis of particle vitiation effects in hypersonic propulsion test facilities
- Development and life prediction of erosion resistant turbine low conductivity thermal barrier coatings
- Development and validation of a multidisciplinary tool for accurate and efficient rotorcraft noise prediction (MUTE)
- Development and validation of a supersonic helium-air coannular jet facility
- Development of a computational aero/fluids analysis system : final report
- Development of a fluid structures interaction test technique for fabrics
- Development of a grid-independent approximate Riemann solver
- Development of an automatic differentiation version of the FPX rotor code
- Development of an axisymmetric afterbody test case for turbulent flow separation validation
- Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations : final technical report
- Development of detonation modeling capabilities for rocket test facilities : hydrogen-oxygen-nitrogen mixtures
- Development of improved surface integral methods for jet aeroacoustic predictions : final report, NASA-Langley grant no. NAG-1660
- Development of the Glenn Heat-Transfer (Glenn-HT) computer code to enable Time-Filtered Navier-Stokes (TFNS) simulations and application to film cooling on a flat plate through long cooling tubes
- Development of three-dimensional DRAGON grid technology
- Development of three-dimensional DRAGON grid technology
- Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination
- Development of tripropellant CFD design code : contract no.--NAS8-40583 : final report
- Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D
- Direct numerical simulation of a temporally evolving incompressible plane wake : effect of initial conditions on evolution and topology
- Direct numerical simulation of incompressible pipe flow using a B-spline spectral method
- Direct numerical simulation of incompressible pipe flow using a b-spline spectral method
- Drag reduction on circular cylinders by ejecting jet from rear stagnation region : progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232
- Dual-pump CARS development and application to supersonic combustion
- Duct flow nonuniformities : effects of struts in SSME HGM II+ : interim report
- Duct flow nonuniformities study for Space Shuttle main engine : technical report
- Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Dynamic stall suppression using combustion-powered actuation (COMPACT)
- Dynamical approach study of spurious steady-state numerical solutions of nonlinear differential equations
- Dynamics of large-scale structures for jets in crossflow
- Dynamics of superfluid helium in low-gravity : NASW-4803, final report
- Effect of coannular flow on linearized Euler equation predictions of jet noise
- Effect of curvature on the impact damage characteristics and residual strength of composite plates
- Effect of turbulence modeling on an excited jet
- Effect of turbulence models on two massively-separated benchmark flow cases
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan
- Effects of rotation on coolant passage heat transfer
- Efficient gradient-based shape optimization methodology using inviscid/viscous CFD : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211
- Efficient grid generation : final report
- Efficient parallel kernel solvers for computational fluid dynamics applications : final report, NASA contract no. NAG1-1672 (Jan. 1995-Aug. 97)
- Energy efficient engine low pressure subsystem flow analysis
- Energy transfer and triadic interactions in compressible turbulence : under contract NAS1-19480
- Engineering aerothermal analysis for X-34 thermal protection system design : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Enhanced multiobjective optimization technique for comprehensive aerospace design : final report on NCC2-5150
- Enhancing aeropropulsion research with high-speed interactive computing
- Entropy splitting and numerical dissipation
- Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing
- Error estimation and uncertainty propagation in computational fluid mechanics
- Essential elements of computational algorithms for aerodynamic analysis and design : under contracts NAS1-97046 & NAS1-19480
- Euler flow computations on non-matching unstructured meshes
- Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts
- Euler technology assessment for preliminary aircraft design : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration
- Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
- Evaluation of CFD turbulent heating prediction techniques and comparison with hypersonic experimental data
- Evaluation of an adaptive unstructured remeshing technique for integrated fluid-thermal-structural analysis
- Evaluation of inflow turbulence methods in large-eddy simulations of a supersonic boundary layer
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeronautics and Astronautics Kissimmee, Florida, January 8-12, 2018
- Exhaust nozzle plume and shock wave interaction
- Exhaust nozzle plume effects on sonic boom test results for isolated nozzles
- Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
- Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
- Experimental and computational aerothermodynamics of a Mars entry vehicle
- Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
- Experimental and computational sonic boom assessment of Boeing N+2 low boom models
- Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models
- Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions
- Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
- Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9
- Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6
- Experimental program for real gas flow code validation at NASA Ames Research Center
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- Extension of a kinetic approach to chemical reactions to electronic energy levels and reactions involving charged species with application to DSMC simulations
- Extension of a streamwise upwind algorithm to a moving grid system
- Extension of a three-dimensional viscous wing flow analysis
- Extension of a three-dimensional viscous wing flow analysis : user's manual : VISTA 3-D code
- Extension of an object-oriented optimization tool : use's reference manual
- Extension of transonic flow computational concepts in the analysis of cavitated bearings
- External boundary conditions for three-dimensional problems of computational aerodynamics
- F-16XL-2 supersonic laminar flow control flight test experiment
- FUN3D manual : 13.6
- FUN3D manual, 12.5
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997
- Final report for the shuttle flight experiment on USMP-4 : in situ monitoring of crystal growth using MEPHISTO
- First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop : proceedings of a workshop held at Langley Research Center, Hampton, Virginia, February 27-29, 1996
- Flamelet model application for non-premixed turbulent combustion : final report under cooperative agreement no. NCCW-75 ...
- Flat plate wake velocity statistics obtained with circular and elliptic trailing edges
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Flight testing the linear aerospike SR-71 experiment (LASRE)
- Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow control under low-pressure turbine conditions using pulsed jets : final report
- Flow distribution around the SSME main injector assembly using porosity formulation
- Flow field characterization of an angled supersonic jet near a bluff body
- Flowfield computation of entry vehicles
- Flowfield-dependent mixed explicit-implicit (FDMEI) algorithm for computational fluid dynamics : final report ...
- Fluid acquisition and resupply experiments on space shuttle flights STS-53 and STS-57
- Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept
- Forced mixer nozzle optimization
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : final technical report
- Fuel injector design optimization for an annular scramjet geometry
- Fundamental ice crystal accretion physics studies
- Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics
- Funding and strategic alignment guidance for infusing small business innovation research technology into NASA programs associated with the Human Exploration and Operations Mission Directorate
- Further development of a method for computing three-dimensional subsonic viscous flows in turbofan lobe mixers
- Further validation of a CFD code for calculating the performance of two-stage light gas guns
- GRID2D/3D, a computer program for generating grid systems in complex-shaped two- and three-dimensional spatial domains
- Generation of performance model for the Aeolian Wind Tunnel (AWT) rotor at reduced pressure
- Geometry and simulation results for a gas turbine representative of the energy efficient engine (EEE)
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- Globalized Newton-Krylov-Schwarz algorithms and software for parallel implicit CFD
- Growth characteristics downstream of a shallow bump : computation and experiment
- Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length
- Heat transfer on a film-cooled rotating blade
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter rotor blade computation in unsteady flows using moving overset grids
- Hierarchical and parallelizable direct volume rendering for irregular and multiple grids
- High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report
- High order finite difference and finite volume WENO schemes and discontinuous Galerkin methods for CFD
- High resolution Euler solvers based on the space-time conservation element and solution element method
- High-order space-time methods for conservation laws
- Higher-order compact schemes for numerical simulation of incompressible flows
- Hopf bifurcation in the driven cavity
- Hydrodynamic design of the fastrac turbopump
- Hypersonic pitching-moment shift for stardust reentry capsule forebody
- ICEG2D (v2.0 : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- ICEG2D--an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice crystal icing research at NASA
- Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Impact of an exhaust throat on semi-idealized rotating detonation engine performance
- Impact of load balancing on unstructured adaptive grid computations for distributed-memory multiprocessors
- Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
- Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
- Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver
- Improvements to an explicit algebraic stress model for turbulent jet mixing predictions
- Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ÌŠangle of attack : contract NAS 3-26617
- Inspection of the Math Model Tools for on-orbit assessment of impact damage report
- Interaction of sound from supersonic jets with nearby structures
- Interactive algebraic grid-generation technique
- Internal passage heat transfer prediction using multiblock grids and a [kappa-omega] turbulence model : under cooperative agreement NCC3-370
- Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Investigation of active flow control to improve aerodynamic performance of oscillating wings
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : final report, Task 1, Ducted propfan analysis
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
- Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
- Isolated rotor forward flight testing at Martian atmospheric density data report
- Jet noise physics and modeling using first-principles simulations
- Jet noise reduction potential from emerging variable cycle technologies
- LES of a jet excited by the Localized Arc Filament Plasma Actuators
- LES, DNS, and RANS for the analysis of high-speed turbulent reacting flows : annual report submitted to NASA Langley Research Center : progress report ... under grant NAG 1-1122 for the period August 1, 1995 - July 31, 1996
- LSPRAY : a Lagrangian spray solver, user's manual : prepared under contract NAS3-27186
- LSPRAY-IV : a lagrangian spray module
- LTCP 2D graphical user interface : application description and user's guide
- Lagrangian approach to jet mixing and optimization of the reactor for production of carbon nanotubes
- Large eddy simulation of transonic flow field in NASA rotor 37
- Large-scale parallel viscous flow computations using an unstructured multigrid algorithm
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Lecture series in computational fluid dynamics
- Linear instability of a uni-directional transversely sheared mean flow
- Long hole film cooling dataset for CFD development, Part 1, Infrared thermography and thermocouple surveys
- Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds
- Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Magnetically actuated propellant orientation experiment, controlling fluid motion with magnetic fields in a low-gravity environment : (MSFC Center Director's Discretionary Fund final report, project no. 93-18)
- Mars entry atmospheric data system modeling, calibration, and error analysis
- Mars sample return : Mars Ascent Vehicle mission & technology requirements
- Mass transfer from a sphere in an oscillating flow with zero mean velocity
- Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report
- Measuring global surface pressures on a circulation control concept using pressure sensitive paint
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- Methods for computationally efficient structured CFD simulations of complex turbomachinery flows
- Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data
- Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept
- Mir cooperative solar array flight performance data and computational analysis
- Mixing enhancement by tabs in round supersonic jets
- Modeling of turbulent swirling flows
- Modeling of unsteady three-dimensional flows in multistage machines
- Modeling the dissipation rate in rotating turbulent flows
- Modeling vortex generators in the Wind-US Code
- Modelling the transitional boundary layer
- Multigrid method for stability problems
- Multiphysics simulation of active hypersonic lip cooling
- Multiprocessing on supercomputers for computational aerodynamics
- NASA N+2 advanced low NOx combustor technology
- NASA Rotor 37 CFD code validation : Glenn-HT code
- NASA numerical and experimental evaluation of UTRC low emissions injector
- NASA one-dimensional combustor simulation : user manual for S1D_ML
- NPSS multidisciplinary integration and analysis
- National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program - 1995 : grant NGT 44-001-800
- National combustion code parallel performance enhancements
- Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing
- Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
- Navier-Stokes simulation of several high-lift reference H configurations
- Navier-Stokes simulation of the crossflow instability in swept-wing flows : a final report to National Aeronautics and Space Administration, Langley Research Center ; submitted by Helen L. Reed
- Near-wall, three-dimensional turbulence measurements : a challenge for laser velocimetry
- Nearly interactive Parabolized Navier-Stokes solver for high speed forebody and inlet flows
- New computational methods for the prediction and analysis of helicopter noise
- Ninth Thermal and Fluids Analysis Workshop proceedings : proceedings of a conference held at ... NASA Glenn Research Center, Cleveland, Ohio, August 31-September 4, 1998
- Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
- Nonlinear dynamics & numerical uncertainties in CFD
- Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel
- Numerical analysis of a rotating detonation engine in the relative reference frame
- Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Numerical assessment of four-part through-flow wave rotor cycles with passage height variation
- Numerical assessment of four-port through-flow wave rotor cycles with passage height variation
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical modeling of spray combustion with an advanced VOF method
- Numerical simulation methods of incompressible flows and an application to the space shuttle main engine
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part I, Fuel nozzle/rich-burn zone analysis
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part II, Quick-quench/lean-combustion zones analysis
- Numerical simulation of complex turbomachinery flows
- Numerical simulation of high-speed turbulent reacting flows : annual report submitted to the NASA Langley Research Center, progress report on activities supported under grant NAG 1-1122 for the period August 1, 1996 - July 31, 1997
- Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Numerical simulation of low-density shock-wave interactions
- Numerical simulation of scramjet inlet flow fields
- Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet
- Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design
- Numerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC
- Numerical solutions of the complete Navier-Stokes equations : final report : NASA grant NAG-1-244
- Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
- Numerical study of stratified charge combustion in wave rotors
- Numerical study of stratified charge combustion in wave rotors
- Numerically simulating an expanding continuum jet into a surrounding non-continuum region
- Object-oriented implementation of the NAS parallel benchmarks using charm++ : annual report
- Observations on computational methodologies for use in large-scale, gradient-based, multidisciplinary design incorporating advanced CFD codes
- Observations regarding use of advanced CFD analysis, sensitivity analysis, and design codes in MDO
- On applications of Chimera grid schemes to store separation
- On approximate factorization schemes for solving the full potential equation
- On approximate factorization schemes for solving the full potential equation
- On convergence acceleration techniques for unstructured meshes
- On formulations of discontinuous Galerkin and related methods for conservation laws
- On multifunctional collaborative methods in engineering science
- On the coupling of CDISC design method with FPX rotor code
- Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements
- Optimization of an advanced design three-element airfoil at high Reynolds numbers
- Orion Service Module Reaction Control System plume impingement analysis using PLIMP/RAMP2
- Overview of ICE project : integration of computational fluid dynamics and experiments
- Overview of ICE project : integration of computational fluid dynamics and experiments
- Overview of heat addition and efficiency predictions for an advanced stirling convertor
- Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project
- PIV and rotational Raman-based temperature measures for CFD validation in a single injector cooling flow
- PLOT3D user's manual
- PLTTER user's guide
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel Newton-Krylov-Schwarz algorithms for the transonic full potential equation : NASA contract no. NAS1-19480
- Parallel implementation of an adaptive scheme for 3D unstructured grids on the SP2
- Parallelization of the implicit RPLUS algorithm : final report, NASA grant NAG 3-1472
- Parallelizing Navier-Stokes computations on a variety of architectural platforms
- Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- Parametric study of decay of homogeneous isotropic turbulence using large eddy simulation
- Particle kinetic simulation of high altitude hypervelocity flight : periodic research report for the period February 1, 1992 - December 31, 1992
- Passive rocket diffuser testing : reacting flow performance of four second-throat geometries
- Passive rocket diffuser theory : a re-examination of minimum second throat size
- Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
- Performance evaluation of the NASA GTX RBCC flowpath
- Performance gains of propellant management devices for liquid hydrogen depots
- Performance impact of deflagration to detonation transition enhancing obstacles
- Performance improvement through indexing of turbine airfoils, Part 2, Numerical simulation
- Performance of the widely-used CFD code OVERFLOW on the Pleides supercomputer
- Physics of forced unsteady separation : proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990
- Planar Inlet Design and Analysis Process (PINDAP)
- Potential application of NASA aerospace technology to ground-based power systems
- Potential application of NASA aerospace technology to ground-based power systems
- Preconditioning for numerical simulation of low Mach number three-dimensional viscous turbomachinery flows
- Preconditioning methods for low-speed flows
- Predicting modes of the unsteady vorticity field near the trailing edge of a blade
- Predicting turbulent convective heat transfer in three-dimensional duct flows
- Predicting turbulent convective heat transfer in three-dimensional duct flows
- Prediction of complex aerodynamic flows with explicit algebraic stress models : 34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV
- Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
- Prediction of relaminarization effects on turbine blade heat transfer
- Preliminary aerodynamic investigation of fan rotor blade morphing
- Preprocessor that enables the use of GridPro grids for unsteady Reynolds-averaged Navier-Stokes code TURBO