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Displaying 1-16 of 16 results
A flying qualities study of longitudinal long-term dynamics of hypersonic planes [microform] / Timothy H. Cox ... [et al.].
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
- 1995
Modeling of longitudinal unsteady aerodynamics of a wing-tail combination [microform] / Vladislav Klein.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile [microform] / Daniel P. Giesy and David M. Christhilf.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
Development of flight testing techniques [microform] : final report, 10/31/79 - 10/31/84 / principal investigator, Doral R. Sandlin.
- Text
- San Luis Obispo, CA : Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
- 1984
Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing [microform] / Dhanvada M. Rao.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
- 1987
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.
- Text
- MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Reduction of Blade-Vortex Interaction (BVI) noise through X-force control [microform] / Fredric H. Schmitz.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration [microform] / W.P. Phillips and W.C. Engelund.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Euler/Navier-Stokes flow computations on flexible configurations for stability analysis [microform] / G. Guruswamy and E. Tu.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1995
Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination [microform] / D.J. Strash and J.M. Summa.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft [microform] / Gerald D. Budd.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
- 1984
Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility [microform] / Peter F. Jacobs and Blair B. Gloss.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS67806Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data [microform] / William T. Suit.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS93085Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Delma C. Freeman, Jr., and Barnard Spencer, Jr.
- 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/gpo71431A flying qualities study of longitudinal long-term dynamics of hypersonic planes / Timothy H. Cox [and three others].
- Text
- Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Facility, April 1995.
- 1995-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo82735
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