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Displaying 1-23 of 23 results
Close-range photogrammetric measurement of static defections for an aeroelastic supercritical wing [microform] / Thomas A. Byrdsong, Richard R. Adams, and Maynard C. Sandford
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
- 1990
Measurements of unsteady pressure and structural response for an elastic supercritical wing [microform] / Clinton V. Eckstrom, David A. Seidel, and Maynard C. Sandford.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1994]
- 1994
Effect of aileron deflections on the aerodynamic characteristics of a semispan model of a subsonic energy-efficient transport [microform] / Peter F. Jacobs.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
- 1985
Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis [microform] : abstract / Gregory W. Burgreen.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995?]
- 1995
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing [microform] / Sheryll Goecke Powers and Lannie D. Webb.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
- 1997
Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration [microform] : proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992 / National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division.
- Text
- Edwards, Calif. : The Division ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
- 1996
Proceedings of the F-8 digital fly-by-wire and supercritical wing first flight's 20th anniversary celebration [microform] : proceedings of an anniversary celebration held at NASA Dryden Flight Research Facility, Edwards, California, May 27, 1992 / symposium Chairman, Kenneth E. Hodge.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1996]
- 1996
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/LPS67806Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction [microform] : semi-annual report for the period March 16, 1983 to September 14, 1983 / by H.T. Nagamatsu, R. Ficarra, R. Orozco.
- Text
- [Hampton, Va.?] : NASA Langley Research Center, [1983]
- 1983
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS86568An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers [microform] / Glynn R. Bartlett.
- Text
- Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
- 1985
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS88314Transonic steady- and unsteady-pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and F.W. Cazier, Jr.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
- 1980
Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and Judith J. Watson.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, [1981]
- 1981
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS97353Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control device [microform] / David A. Seidel, Maynard C. Sanford and Clinton V. Eckstrom.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
- 1985
Numerical calculation of the transonic potential flow past a cranked wing [microform] / I-Chung Chang and Michael Tauber.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
- 1983
Geometric and structural properties of a rectangular supercritical wing oscillated in pitch for measurement of unsteady transonic pressure distributions [microform] / Rodney H. Ricketts ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
- 1983
Transonic calculations for a flexible supercritical wing and comparison with experiment [microform] / Robert M. Bennett, David A. Seidel, Maynard C. Sandford.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
- 1985
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/gpo65701Physical properties of the Benchmark Models Program supercritical wing / Bryan E. Dansberry [and five others].
- Text
- Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, September 1993.
- 1993-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo173159A theory of supercritical wing sections, with computer programs and examples [by] F. Bauer, P. Garabedian [and] D. Korn.
- Text
- Berlin, New York, Springer-Verlag, 1972.
- 1972
- 1 Item
Item details Format Call Number Item Location Text TL571.B38 Off-site Supercritical wing sections III / Frances Bauer, Paul Garabedian, David Korn.
- Text
- Berlin ; New York : Springer-Verlag, 1977.
- 1977
- 1 Item
Item details Format Call Number Item Location Text TL570 .B365 Off-site Supercritical wing sections II : a handbook / Frances Bauer ... [et al.].
- Text
- Berlin ; New York : Springer-Verlag, 1975.
- 1975
- 1 Item
Item details Format Call Number Item Location Text TL571.S82 Off-site A theory of supercritical wing sections, with computer programs and examples [by] F. Bauer, P. Garabedian [and] D. Korn.
- Text
- Berlin, New York, Springer-Verlag, 1972.
- 1972
- 1 Item
Item details Format Call Number Item Location Text TL571.B38 Off-site
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