Research Catalog
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Displaying 1-4 of 4 results
An axisymmetric analog two-layer convective heating procedure with application to the evaluation of space shuttle orbiter wing leading edge and windeward surface heating [microform] / K.C. Wang.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
- 1994
Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment [microform] / Herbert J. Gladden and Matthew E. Melis.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions [microform] / William A. Wood.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions / Joseph G. Marvin, James L. Brown, Peter A. Gnoffo.
- Text
- Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, November 2013.
- 2013-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54962
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