A nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison / by Robert L. Trimpi and Nathaniel B. Cohen.
The linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the...
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| Main Authors: | , |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
1961.
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| Series: | NASA technical report ;
R-85. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.12:85
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| NAS 1.12:85 | Available Place a Hold |