You need to sign in or sign up before continuing.

Experimental Studies of Hypersonic Shock-Wave Boundary-Layer Interactions by National Aeronautics and Space Adm Nasa

Experimental Studies of Hypersonic Shock-Wave Boundary-Layer Interactions

National Aeronautics and Space Adm Nasa

66 pages missing pub info (view editions)

nonfiction science emotional medium-paced
Powered by AI (Beta)
Loading...

Description

Two classes of shock-wave boundary-layer interactions were studied experimentally in a shock tunnel in which a low Reynolds number, turbulent flow at Mach 8 was developed on a cold, flat test surface. The two classes of interactions were: (1) a sw...

Read more

Community Reviews

Loading...

Content Warnings

Loading...