Research Catalog
New! Try our Article Search to discover online journals, books, and more from home with your library card.
Displaying 1-6 of 6 results
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.
- Text
- Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls [microform] : final technical report, grant #NAG 2-789 / Jan Roskam, principal investigator, Deane E. Ackers.
- Text
- Lawrence, Kan. : University of Kansas, Center for Research, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Pressure measurements of impinging jet with asymmetric nozzle : progress report / principal investigator: Ho, Chih-Ming.
- Text
- Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
- 1988
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS112097Pressure measurements of impinging jet with asymmetric nozzle [microform] : progress report / principal investigator: Ho, Chih-Ming.
- Text
- Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
- 1988
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS112097Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / Frank J. Kurtenbach and Frank W. Burcham, Jr.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
- 1981-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo71438
No results found from Digital Research Books Beta
Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.
