The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 / John, J. Gawienowski.
|Main Author:||Gawienowski, John J.|
Washington, D.C. : National Aeronautics and Space Administration, 1961.
Boundary layer control.
Cone > Aerodynamics.
Wind tunnel testing.
Full text also available online. Address as of 11/15/2010:
23 p. :
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