Research Catalog
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Displaying 1-6 of 6 results
Estimated benefits of variable-geometry wing camber control for transport aircraft [microform] / Alexander Bolonkin, Glenn B. Gilyard.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
High-lift systems on commercial subsonic airliners [microform] / Peter K.C. Rudolph.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances [microform] / Lisa J. Bjarke.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS59777The Concorde and aeronautical research [microform] / M. Salmon.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, [1982]
- 1982
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing / Sheryll Goecke Powers and Lannie D. Webb.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
- 1997-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo65701
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