Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime PDF Download

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Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime

Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime PDF Author: Roger M. Winebarger
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 28

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