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Drag and heat transfer on surfaces with small longitudinal finsAn investigation is conducted regarding the drag characteristics of longitudinally ribbed surfaces using various configurations which attempt to confine the turbulent wall bursts to regions of small transverse extent in the initial birth region. The ratio of heat transfer increase to drag increase for the high area ratio rib configurations is determined and the heat transfer efficiency of the present surfaces is compared with data found in the literature. The drag data obtained indicate local 'wetted area skin friction' reductions but due to the increased surface area the planform drag is increased in most instances. There is no indication of drag reduction with the rectangular ribbed models that had sharp leading and fin tip edges. Heat transfer data indicate that several of the triangular grooved models have efficiencies approximately 10 percent higher than that of a smooth flat plate.
Document ID
19780057951
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walsh, M. J.
(NASA Langley Research Center Hampton, VA, United States)
Weinstein, L. M.
(NASA Langley Research Center High-Speed Aerodynamics Div.; Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 78-1161
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Seattle, WA
Start Date: July 10, 1978
End Date: July 12, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A41860
Distribution Limits
Public
Copyright
Other

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