Research Catalog
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Displaying 1-17 of 17 results
Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel [microform] / Sharon S. Graves.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration [microform] / Bryan A. Campbell, Zachary T. Applin, and Guy T. Kennerly.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
- 1999
Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms [microform] / Kevin J. Kjerstad ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
- 1999
Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport [microform] / Guy T. Kemmerly ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
- 1999
Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
- 1999
Modification of the Ames 40- by 80-foot wind tunnel for component acoustic testing for the second generation supersonic transport [microform] / F.H. Schmitz, J.R. Allmen, and P.T. Soderman.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Study of the unsteady flow features on a stalled wing [microform] / S. Yon and J. Katz.
- Text
- Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel [microform] / Norbert Ulbrich.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel [microform] / Victor A. Canacci, Jose C. Gonsalez, and David A. Spera.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users [microform] / Garl L. Gentry, Jr. ... [et al.].
- 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], 1990.
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS65627Development and application of dynamic simulations of a subsonic wind tunnel [microform] / John R. Szuch, ... [et al.].
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Progress in the Lewis Research Center altitude wind tunnel (AWT) modeling program [microform] / Carl C. Ciepluch ... [et al.].
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Remarks on the layout of the subsonic free jet wind tunnels [microform] / Jorg-Dieter Vagt.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, [1983]
- 1983
Experimental investigation of an ejector-powered free-jet facility [microform] / Mary Jo Long.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1992]
- 1992
Data reduction functions for the Langley 14- by 22-foot subsonic tunnel / Andy D. Boney.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2014.
- 2014-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54991Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover / Anthony Neal Watkins [and five others].
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2018.
- 2018-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo11159414- by 22-foot subsonic tunnel laser velocimeter upgrade / James F. Meyers [and three others].
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37522
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