NASA Dryden Flight Research Center
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The organization NASA Dryden Flight Research Center represents an institution, an association, or corporate body that is associated with resources found in University of Missouri Libraries.
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NASA Dryden Flight Research Center
Resource Information
The organization NASA Dryden Flight Research Center represents an institution, an association, or corporate body that is associated with resources found in University of Missouri Libraries.
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- NASA Dryden Flight Research Center
78 Items by the Organization NASA Dryden Flight Research Center
8 Items that are about the Organization NASA Dryden Flight Research Center
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- [Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests]
- A comparison of hypersonic vehicle flight and prediction results
- A conversion of Wheatstone bridge to current-loop signal conditioning for strain gages
- A correlation between flight-determined derivatives and wind-tunnel data for the X-24B research aircraft
- A historical overview of flight flutter testing
- A model for space shuttle orbiter tire side forces based on NASA landing systems research aircraft test results
- A presentation on robust flutter margin analysis and a flutterometer
- A reassessment of heavy-duty truck aerodynamic design features and priorities
- Aeroservoelastic uncertainty model identification from flight data
- An electronic workshop on the performance seeking control and propulsion controlled aircraft results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program : proceedings of the electronic workshop
- An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
- An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft
- An overview of the NASA F-18 high alpha research vehicle
- Atmospheric considerations for uninhabited aerial vehicle (UAV) flight test planning
- CFD analysis of nozzle jet plume effects on sonic boom signature
- Coherent lidar turbulence measurement for gust load alleviation
- Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Data synchronization discrepancies in a formation flight control system
- Design and calibration of the X-33 flush airdata sensing (FADS) system
- Design and development of an F/A-18 inlet distortion rake : a cost and time saving solution
- Design and integration of an actuated nose strake control system
- Developing uncertainty models for robust flutter analysis using ground vibration test data
- Recent flight test experience with uninhabited aerial vehicles at the NASA Dryden Flight Research Center
- Reconfigurable control design for the full X-33 flight envelope
- Robust flutter margin analysis that incorporates flight data
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Selected examples of NACA/NASA supersonic flight research
- Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle
- Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis
- Supersonic flying qualities experience using the SR-71
- The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned
- Theoretical and experimental investigations of sensor location for optimal aeroelastic system state estimation
- Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
- User's guide for SKETCH
- User's guide for computer program that routes signal traces
- Using engine thrust for emergency flight control : MD-11 and B-747 results
- Visualization of in-flight flow phenomena using infrared thermography
- Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data
- Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane
- Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8
- Development of the X-33 aerodynamic uncertainty model
- Dynamic ground effect for a cranked arrow wing airplane
- Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers
- Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers
- Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data
- Exploring the extreme : high performance learning activities in mathematics, science and technology
- Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
- F-15B/flight test fixture II : a test bed for flight research
- F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
- F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack : contract NAS 3-26617
- Fifty years of flight research : an annotated bibliography of technical publications of NASA Dryden Flight Research Center, 1946-1996
- Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Flight simulation software at NASA Dryden Flight Research Center
- Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
- Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodies
- Flying quality analysis of a JAS 39 Gripen ministick controller in an F/A-18 aircraft
- Ground-based sensors for the SR-71 sonic boom propagation experiment
- In-flight transport performance optimization : an experimental flight research program and an operational scenario
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack : contract NAS 3-26617
- Large-deformation displacement transfer functions for shape predictions of highly flexible slender aerospace structures
- Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft
- Mathematical analysis study for radar data processing and enhancement
- Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts
- Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains
- Nonstationary dynamics data analysis with wavelet-SVD filtering
- Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces
- Operational concepts for uninhabited tactical aircraft
- Overview of recent flight flutter testing research at NASA Dryden
- Pilot-induced oscillation research : the status at the end of the century
- Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods
- Production support flight control computers : research capability for F/A-18 aircraft at Dryden Flight Research Center
- Propulsion flight research at NASA Dryden from 1967 to 1997
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- Developing uncertainty models for robust flutter analysis using ground vibration test data
- Coherent lidar turbulence measurement for gust load alleviation
- Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8
- Reconfigurable control design for the full X-33 flight envelope
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack
- Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains
- Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers
- Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests
- Design and integration of an actuated nose strake control system
- Large-deformation displacement transfer functions for shape predictions of highly flexible slender aerospace structures
- Nonstationary dynamics data analysis with wavelet-SVD filtering
- Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft
- F-15B/flight test fixture II : a test bed for flight research
- Mathematical analysis study for radar data processing and enhancement
- F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.missouri.edu/resource/LZd6AvYpFC0/" typeof="Organization http://bibfra.me/vocab/lite/Organization"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.missouri.edu/resource/LZd6AvYpFC0/">NASA Dryden Flight Research Center</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.missouri.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.missouri.edu/">University of Missouri Libraries</a></span></span></span></span></div>
