Experimental study of pressure and heating rate on a swept cylindrical leading edge resulting from swept shock wave interference [microform] / by Christopher E. Glass.
Published
[Washington, D.C.? : National Aeronautics and Space Administration, 1989]
Physical Description
1 v.
Notes
Distributed to depository libraries in microfiche.
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches.