Research Catalog
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Displaying 1-32 of 32 results
IMPAC--an Integrated Methodology for Propulsion and Airframe Control [microform] / Sanjay Garg ... [et al.].
- Text
- [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1991?]
- 1991
Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft [microform] / submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.
- Text
- Cleveland, OH : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Multiple-purpose subsonic naval aircraft (MPSNA) : multiple application propfan study (MAPS) [microform] / D.M. Winkeljohn, C.H. Mayrand.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
Cooperative control theory and integrated flight and propulsion control [microform] : final report for grant NAG3-998 covering the period 1990-1993 / by David K. Schmidt and John D. Schierman.
- Text
- College Park, Md. : Dept. of Aerospace Engineering, University of Maryland ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
V/STOL aircraft configurations and opportunities in the Pacific Basin [microform] / James A. Albers and John Zuk.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
- 1987
Flightpath synthesis and HUD scaling for V/STOL terminal area operations [microform] / Vernon K. Merrick and James A. Jeske.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests [microform] / Helen E. Kourous and Richard G. Seasholtz.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight [microform] / Sanjay Garg ... [et al.] ; prepared for the Guidance, Navigation and Control Conference sponsored by the American Institute of Aeronautics and Astronautics, Portland, Oregon, August 20-22, 1990.
- Text
- [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
- 1990
Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover [microform] / James A. Franklin and Michael W. Stortz.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
The attributes of a variable-diameter rotor system applied to civil tiltrotor aircraft [microform] : NASA university consortium grant NCC2-5174 / by Scott Brender, Hans Mark, and Frank Àguilera.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
V/STOL dynamics, control, and flying qualities [microform] / James A. Franklin.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
- 2000
Suckdown, fountain lift, and pressures induced on several tandem jet V/STOL configurations [microform] / David C. Bellavia ... [et al.].
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
- 1991
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS58956Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques [microform] / Sanjay Garg and Peter J. Ouzts.
- Text
- [Cleveland, Ohio : Lewis Research Center, 1991]
- 1991
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS64062Supersonic flow computations for an ASTOVL aircraft configuration [microform] : phase 2, part 2 / Sekaripuram Ramakrishnan, Sukumar R. Chakravarthy, and Kuo-Yen Szema.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1990.
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS67904Computer simulation of a pilot in V/STOL aircraft control loops. Appendix II, The optimal control model of a pilot in V/STOL aircraft control loops [microform] / principal investigators: William G. Vogt, Marlin H. Mickle.
- Text
- Cleveland, OH : NASA Lewis Research Center, [1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS69059Computer simulation of a pilot in V/STOL aircraft control loops. Appendix III, The adaptive control model of a pilot in V/STOL aircraft control loops [microform] / principal investigators: William G. Vogt, Marlin H. Mickle.
- Text
- Cleveland, OH : NASA Lewis Research Center, [1988]
- 1988
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS69060Analysis of internal flow in a ventral nozzle for STOVL aircraft [microform] / C. Frederic Smith and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.
- Text
- [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS69189Research on a two-dimensional inlet for a supersonic V/STOL propulsion system [microform] / by J.L. Mark, M.A. McGarry, and P.V. Reagan.
- Text
- St. Louis, Mo.] : McDonnell Aircraft Company, McDonnell Douglas Corporation ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS71139Ground effects on V/STOL and STOL aircraft--a survey [microform] / Richard E. Kuhn, James Eshleman.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
- 1985
A flight-test methodology for identification of an aerodynamic model for a V/STOL aircraft [microform] / Ralph E. Bach, Jr., B. David McNally.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1988]
- 1988
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS93229V/STOL maneuverability and control [microform] / James A. Franklin and Seth B. Anderson.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
- 1984
V/STOL wind-tunnel testing [microform] / David G. Koenig.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
- 1984
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS95840Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft [microform] / W. P. Nelms.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
- 1984
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS95844V/STOL concepts in the the United States [microform] : past, present, and future / W.P. Nelms and S. B. Anderson.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
- 1984
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS95848Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines [microform] / Leo C. Franciscus and Roger W. Luidens.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1984]
- 1984
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS99531Analytical study of blowing boundary-layer control for subsonic V/STOL inlets [microform] / Danny P. Hwang.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1984]
- 1984
Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles [microform] / H.C. Kao, P. L. Burstadt, and A. L. Johns.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1984]
- 1984
Tandem fan applications in advanced STOVL fighter configurations [microform] / Charles L. Zola and Samuel B. Wilson, III and Megan A. Eskey.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1984]
- 1984
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS99551V/STOL model fan rig, design report [microform] / [ J. G. Cheatham, T. L. Creason].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1983]
- 1983
Preliminary experiments on the noise generated by target-type thrust reverser models / by Orlando A. Gutierrez and James R. Stone.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, May 1972.
- 1972-5
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo173326An overview of the quiet short-haul research aircraft program / Michael D. Shovlin and John A. Cochrane.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, November 1978.
- 1978-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo173549
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