Research Catalog
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Displaying 1-11 of 11 results
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
Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system [microform] / Daniel W. Banks and John W. Paulson.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
- 1987
Stress analysis of Pathfinder-II models [microform] / S.C. Mehrotra and C.T.L. Mills.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
- 1984
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Application of particle image velocimetry to a study of flow about a multi-element airfoil [microform] : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155 / by the Department of Aeronautics and Astronautics, Stanford University ; Stephen M. Walker; Donald Baganoff, principal investigator.
- Text
- Stanford, Calif. : Dept. of Aeronautics and Astronautics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
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
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program [microform] / Bruce Charles.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap [microform] / Ahmed Hassan.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / Gary E. Erickson.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo40579AFC-enabled simplified high-lift system integration study / Peter M. Hartwich [and seven others].
- Text
- Hampton, Virginia. : National Aeronautics and Space Administration, Langley Research Center, September 2014.
- 2014-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54809
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