F-15 aircraft
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The concept F-15 aircraft represents the subject, aboutness, idea or notion of resources found in University of Missouri Libraries.
The Resource
F-15 aircraft
Resource Information
The concept F-15 aircraft represents the subject, aboutness, idea or notion of resources found in University of Missouri Libraries.
- Label
- F-15 aircraft
- Source
- nasat
25 Items that share the Concept F-15 aircraft
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- The high stability engine control (HISTEC) program : flight demonstration phase
- A comparison of time-optimal interception trajectories for the F-8 and F-15 : final report
- A preliminary evaluation of an F100 engine parameter estimation process using flight data
- Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem
- CFD analysis of nozzle jet plume effects on sonic boom signature
- Conversion from engineering units to telemetry counts on Dryden Flight simulators
- Development and flight evaluation of an emergency digital flight control system using only engine thrust on an F-15 airplane
- Direct adaptive aircraft control using dynamic cell structure neural networks
- Dynamic ground effect for a cranked arrow wing airplane
- Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
- Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
- F-15B/flight test fixture II : a test bed for flight research
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility
- Full flight envelope direct thrust measurement on a supersonic aircraft
- High stability engine control (HISTEC) flight test results
- High stability engine control (HISTEC) flight test results
- In-flight boundary-layer transition on a large flat plate at supersonic speeds
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- Optimal cooperative control synthesis of active displays
- Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane
- Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine
- The high stability engine control (HISTEC) program : flight demonstration phase
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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/hNhA1ydKCyE/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.missouri.edu/resource/hNhA1ydKCyE/">F-15 aircraft</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>
