Research Catalog
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Displaying 1-15 of 15 results
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service (NTIS) [distributor, 1995]
- 1995
Investigation into the impact of agility in conceptual fighter design [microform] / R.M. Engelbeck.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law [microform] / Jessie C. Yeager.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis [microform] / Bruce G. Powers.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
- 1996
High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle [microform] / Keith D. Wichman ... [et al.].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
- 1996
Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
- 2000
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS23428Candidate control design metrics for an agile fighter [microform] / Patrick C. Murphy, Melvin L. Bailey, Aaron J. Ostroff.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
- 1991
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS60321Subsonic flow investigations on a cranked wing designed for high maneuverability / Dhanvada M. Rao.
- Text
- Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27947Subsonic flow investigations on a cranked wing designed for high maneuverability [microform] / Dhanvada M. Rao.
- Text
- Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis / Bruce G. Powers.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1996.
- 1996-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo65385High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle / Keith D. Wichman [and six others]
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1996.
- 1996-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo65674Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability / Steven M. Sliwa.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
- 1980-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo71360Airfoil dynamic stall and rotorcraft maneuverability / William G. Bousman.
- Text
- Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2000.
- 2000-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS23428Semi-annual status report on NASA grant NAG 1-1087 : "identification of aerodynamic models for maneuvering aircraft" / by Suei Chin and C. Edward Lan.
- Text
- Lawrence, Kan. : Flight Research Laboratory, The University of Kansas Center for Research, Inc., [1990]
- 1990
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS60899
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