Experimental Investigation of Contraction Ratio Influence on Scramjet Inlet Performance at Mach 5.85

Experimental Investigation of Contraction Ratio Influence on Scramjet Inlet Performance at Mach 5.85

Bibliographic Details
Main Author:	Linton, Megan Marie
Language:	English
Published:	University of Dayton / OhioLINK 2021
Subjects:	Aerospace Engineering Busemann inlet scramjet inlet performance hypersonic performance test contraction ratio
Online Access:	http://rave.ohiolink.edu/etdc/view?acc_num=dayton1620301711347689

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