The investigation of the flow in the vicinity of V shaped wings formed by stream surfaces behind a plane shock wave
By: by V. V. Keldysh. [Translated by J. W. Palmer]
Series: Royal Aircraft Establishment. Library translation no. 1407
Publisher: Ministry of Technology
Published: 1969
Place of publication: Farnborough [Eng.]
Language: eng
Subjects: Aerodynamics, Supersonic.; Airplanes -- Wings, Swept-back.; Shock waves.
Notes: Includes bibliography.
Cover title.
"Mekhanika Zhidkosti i Gaza, 4, pp. 50-55 (1967)"