Research Catalog
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Displaying 1-3 of 3 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
Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability [microform] / Linda S. Bangert and Laurence D. Leavitt.
- 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/LPS60139Flight test results from the rake airflow gage experiment on the F-15B airplane / Michael A. Frederick and Nalin A. Ratnayake.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
- 2011
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo30629
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