With aid of method of small oscillations, excitation of unstable perturbations for Hartree velocity distributions occurring in plane boundary layer flow for decreasing and increasing pressure is calculated; contribution toward calculation of transition point on cylindrical bodies. English Translation from Jahrbuch der deutschen Luftfahrtforschung Aug 1942.
Excitation of unstable perturbations in laminar friction layer
NACA -- Tech Memo
1952
63 pages
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Article (Journal)
English
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Estimate of slip effect on compressible laminar-boundary-layer skin friction
Engineering Index Backfile | 1952
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