Experimental Investigation of the Effects of Support Interference on the Pressure Distribution of a Body of Revolution at a Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 14 x 10(exp 6)
A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented. (author)
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Zusammenfassung: | A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented. (author) |
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