Numerical solution for the interaction of shock wave with laminar boundary layer in two-dimensional flow in a flat plate
By: Uriel Landau
Contributors: United States. National Aeronautics and Space Administration; Leo Kanner Associates
Series: NASA technical memorandum -- 77408
Publisher: National Aeronautics and Space Administration
Published: 1984
Place of publication: Washington, D.C
Language: eng
Format: Microform
Subjects: Boundary layer; Two-phase flow
Work titles: Pitron numeri shel ha-interaḳzyah ben shikhvat gevul laminarit le-ben gal-helem bi-zerimah du-memadit ʻal luaḥ shatuaḥ.
Notes: "Leo Kanner Associates"--Std. t.p

Translation of Pitron numeri shel ha'interakziyah beyn shikhvat g'vool laminarit le'beyn gal-hailem be's'reemah doo-meymadit al loo'akh shatoo'akh, Ph.D. research thesis, Technicon, Israel Institute of Technology, Haifa, June 1976, 191 pp

"April 1984."

"N84-29160"--Microfiche header

Bibliography: p. 135-142

Translation

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 3 microfiches ; 11 x 15 cm

National Aeronautics and Space Administration. NASw-3541