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Aerodynamic Performance of Several Techniques for Spike-position Control of a Blunt-lip Nose Inlet Having Internal Contraction; Mach Numbers of 0.63 and 1.5 to 2.0
Authors
Arthur A Anderson
Maynard I Weinstein
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
