Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers PDF Download

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Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers

Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers PDF Author: Richard D. Samuels
Publisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82

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