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.
"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.