Curvature-Driven Favorable Pressure Gradient Effects on Shock Boundary Layer Interactions /

Bibliographic Details
Main Author:	Carlson, Joseph Douglas (Author)
Other Authors:	Tichenor, Nathan (Thesis advisor), Bowersox, Rodney (Thesis advisor)
Format:	Thesis eBook
Language:	English
Published:	[College Station, Texas] : [Texas A&M University], [2023]
Subjects:	Major Aerospace Engineering supersonic hypersonic scramjet engine aerodynamics propulsion SBLI separation favorable pressure, gradient
Online Access:	Link to OAKTrust Copy

Link to OAKTrust Copy

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Notes:		Available via Institutional Repository (OAKTrust)

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