Analysis of Hypersonic Boundary Layer Second Mode Instability over a 7° Cone

This paper presents the results of the analysis of Mach 8.0 flow over a seven degree half-angle cone. The purpose of this analysis was to develop techniques to examine boundary layer transition at hypersonic velocities. The specific objectives were to look for second mode instability waves character...

Бүрэн тодорхойлолт

Номзүйн дэлгэрэнгүй

Үндсэн зохиолч:	Dennery, Richard A.
Формат:	text
Хэвлэсэн:	AFIT Scholar 1994
Нөхцлүүд:	Boundary layer Hypersonic aerodynamics Aerodynamics and Fluid Mechanics
Онлайн хандалт:	https://scholar.afit.edu/etd/6328 https://scholar.afit.edu/context/etd/article/7331/viewcontent/AFIT_GA_ENY_94D_20_Dennery_R_ADA289471_Redacted.pdf
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