Research Catalog
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Displaying 1-4 of 4 results
Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
- 1988
Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails [microform] / Jerry M. Allen and Carolyn B. Watson.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds [microform] / M. Leroy Spearman.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
Missile aerodynamics for ascent and re-entry / G.L. Watts, J.W. McCarter.
- Text
- Huntsville, Alabama : National Aeronautics and Space Administration, Langley Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37318
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