Steady/oscillatory, supersonic/hypersonic inviscid flow past oscillating wings and wedge combinations at arbitrary angles of attack
Publisher: Naval Postgraduate School
Published: 1981
Place of publication: Monterey, California
Language: eng
Subjects: Aeronautics
Notes: ADA107438.

Thesis (M.S. in A.E. and Degree of A. Engineer)--Naval Postgraduate School, 1981.

Bibliography: l. 180.