Laminar boundary-layer separation induced by flares on cylinders at zero angle of attack / by Donald M. Kuehn.
Laminar boundary-layer separation induced by a flare on a cylindrical body of revolution has been experimentally investigated in the Mach number range of 2.0 to 5.5. The Reynolds number range (based on boundary-layer thickness) was 1x10³ to 30x10³. Geometric variables were nose shape, cylinder lengt...
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
1962.
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| Series: | NASA technical report ;
R-146. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.12:146
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| NAS 1.12:146 | Available Place a Hold |