The influence of the boundary layer on the character of the flow of gas in a tube behind a moving shock wave
By: Yu A. Dem'yanov.
Contributors: Royal Aircraft Establishment (Great Britain)
Series: Royal Aircraft Establishment. Library translation -- no. 796
Publisher: Royal Aircraft Establishment
Published: 1959
Place of publication: Farnborough, Hants
Notes: Original Russian source : Prikladnaya matematika i mekhanika, 21 (1957) 4, p.473-477.

Bibliographical references: p.9.