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Author Dodbele, S. S.

Title Effects of forebody geometry on subsonic boundary-layer stability [electronic resource] / S. S. Dodbele.

Imprint [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.


Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4314    ---  Available
Description 17 p. : ill. ; 28 cm.
Series NASA contractor report ; 4314
NASA contractor report ; NASA CR-4314
Note "Prepared for Langley Research Center under contract NAS1-17919."
Presented as a paper at the 5th International Conference on Numerical Methods in Laminar and Turbulent Flow, Montreal, Quebec, Canada, July 6-10, 1987.
Form Mode of access via the NTRS web site.
Bibliography Bibliography: p. 14-17.
Subject Boundary layer.
Laminar flow.
Noses (Aircraft)
Boundary layer stability.
Flow geometry.
Laminar boundary layer.
Subsonic flow.
Added Author Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
International Conference on Numerical Methods in Laminar and Turbulent Flow (5th : 1987 : Montreal, Quebec)
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:4314

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