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This content will become publicly available on January 3, 2026

Title: Stability Investigations of Mach 5.35 Boundary Layer Flow Over Distributed Roughness
Award ID(s):
2146100
PAR ID:
10581073
Author(s) / Creator(s):
; ;
Publisher / Repository:
American Institute of Aeronautics and Astronautics
Date Published:
ISBN:
978-1-62410-723-8
Format(s):
Medium: X
Location:
Orlando, FL
Sponsoring Org:
National Science Foundation
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