Experimental study of pressure and heating rate on a swept cylindrical leading edge resulting from swept shock wave interference
By: by Christopher E. Glass.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-185326.
Publisher: National Aeronautics and Space Administration
Published: 1989
Place of publication: [Washington, D.C.?
Language: eng
Format: Microform
Subjects: Leading edges (Aerodynamics); Interference (Aerodynamics)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches.