Supersonic turbulent boundary-layer flows with mass injection through slots and/or porous walls /
An implicit finite-difference method was used to solve the compressible boundary-layer equations, and to study the effects of mass transfer through porous plates, slots, and a combination of the two. The effects of the external pressure field were also included by using a global pressure interaction...
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| Corporate Authors: | , |
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| Format: | Book |
| Language: | English |
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Washington :
National Aeronautics and Space Administration,
1975
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1975 |
| Series: | NASA contractor report
NASA CR-2587 |
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