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  5. Experimental Studies of Shock Train Generation and Unstart Propagation in Mach 2.3 Flow
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Experimental Studies of Shock Train Generation and Unstart Propagation in Mach 2.3 Flow

Date Issued
May 1, 2024
Author(s)
Bartlett, Nicholas W  
Advisor(s)
Trevor M. Moeller
Additional Advisor(s)
Trevor M. Moeller, Phillip Kreth, Cary Smith, James Simonton
Abstract

Abstract withheld because of embargo that is in place.

Subjects

Unstart

Shock Train

Unsteadiness

Mach 2.3

Back Pressure

Scramjet

Disciplines
Aerodynamics and Fluid Mechanics
Aerospace Engineering
Degree
Master of Science
Major
Aerospace Engineering
Embargo Date
May 15, 2030

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