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NASA NTRS · 19660039520

Effect of boundary-layer transition on dynamic stability.

Jaffe, P.·Prislin, R. H.

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Abstract

Free flight dynamic stability measurements indicate that boundary layer transition has no perceptible effect

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WIND TUNNEL STABILITY TEST BOUNDARY LAYER TRANSITION FREE FLIGHT TEST APPARATUS AERODYNAMIC STABILITY

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Jaffe, P., Prislin, R. H.. 1966-01-01. Effect of boundary-layer transition on dynamic stability.. https://ntrs.nasa.gov/citations/19660039520

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