Item Details

Effects of Forebody Geometry on Subsonic Boundary-Layer Stability

S.S. Dodbele
Format
Book; Government Document; Online; EBook
Published
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.
Language
English
Series
NASA Contractor Report
Description
17 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Presented as a paper at the 5th International Conference on Numerical Methods in Laminar and Turbulent Flow, Montreal, Quebec, Canada, July 6-10, 1987.
  • Prepared at Vigyan Research Associates, Inc., for Langley Research Center under Contract NAS1-17919.
  • Bibliography: p. 14-17.
Series Statement
NASA contractor report ; 4314
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Presented as a paper at the 5th International Conference on Numerical Methods in Laminar and Turbulent Flow, Montreal, Quebec, Canada, July 6-10, 1987.
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