Effect Of Boundary Layer Profile, Air Speed, And System Geometry On The Stability Of Flow In Suction Systems

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Report Number: WADC TR 55-318
Author(s): Treanor, C. E., Flax, A. H.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-07
Pages: 56
Contract: AF 33(616)-2373
DoD Project: 1366
DoD Task: 70103
PB Number: PB134658
Identifier: AD0097115

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Provenance: Lockheed Martin Missiles & Fire Control

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