Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
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Author
Contributions
- Wang, Kon-Sheng Charles. - Contributor
- NASA Dryden Flight Research Center. - Contributor
Publication
1997 - National Aeronautics and Space Administration, Dryden Flight Research Center, Edwards, Calif, California
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number42758582
- Open LibraryOL17591853M
Alternate Titles
- Flight determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring.
Subjects
Topics
AirplanesFlight testsControl systemsAngle of attackAircraft controlControl surfacesResearch vehiclesUnsteady aerodynamicsThrust vector controlYawing (Aerodynamics)Longitudinal stabilityParameter identificationHornet (Jet fighter plane)Maximum likelihood estimatesAngle of attack (Aerodynamics)Longitudinal Stability of airplanes
Series Statement
- [NASA technical paper] -- NASA/TP-97-206539.
- NASA technical paper -- 206539.
Other Editions
- Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
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