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Effect of boundary-layer transition on dynamic stability.Free flight dynamic stability measurements indicate that boundary layer transition has no perceptible effect
Document ID
19660039520
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jaffe, P.
Prislin, R. H.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 64-427
Report Number: AIAA PAPER 64-427
Accession Number
66A18810
Distribution Limits
Public
Copyright
Other
Keywords
WIND TUNNEL STABILITY TEST
BOUNDARY LAYER TRANSITION
FREE FLIGHT TEST APPARATUS
AERODYNAMIC STABILITY

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