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Displaying 1-4 of 4 results
A spectrally accurate boundary-layer code for infinite swept wings [microform] / C. David Pruett.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1994
Computational study of flow establishment in hypersonic pulse facilities [microform] / S. Yungster, K. Radhakrishnan.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Asymptotic analysis of numerical wave propagation in finite difference equations / by Michael Giles, W.T. Thompkins, Jr.
- Text
- Cambridge, Massachusetts : Gas Turbine & Plasma Dynamics Laboratory, Massachusetts Institute of Technology, 1983.
- 1983
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo50357Asymptotic analysis of numerical wave propagation in finite difference equations / by Michael Giles, W.T. Thompkins, Jr.
- Text
- Cambridge, Massachusetts : Gas Turbine & Plasma Dynamics Laboratory, Massachusetts Institute of Technology, 1983.
- 1983
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