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Transition caused by the laminar flow separationAn experimental investigation of the effects of the geometry of body surface, Reynolds number, stream turbulence, and a roughness element (wire) on the reattachment of separated laminar boundary-layer flow on a bent flat plate is presented and discussed. The flow mechanisms determining reattachment of the boundary layer are analyzed and discussed.
Document ID
19930093878
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Maekawa, T
Atsumi, Shoichi
Date Acquired
August 16, 2013
Publication Date
September 1, 1952
Report/Patent Number
NACA-TM-1352
Report Number: NACA-TM-1352
Accession Number
93R23203
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER CHARACTERISTICS - WING SECTIONS
BOUNDARY LAYER TRANSITION - EFFECT OF TURBULENCE
BOUNDARY LAYER TRANSITION
BOUNDARY LAYER TRANSITION - EFFECT OF PRESSURE GRADIENT
THEORIES - BOUNDARY LAYER
REYNOLDS NUMBER EFFECTS - WING SECTIONS
BOUNDARY LAYER TRANSITION - EFFECT OF SURFACE ROUGHNESS
BOUNDARY LAYER SEPARATION
FLOW, TURBULENT
FLOW, LAMINAR

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