Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (The Efficiency of Shock Diffusers)-Reference-Cited by-同舟云学术

Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (The Efficiency of Shock Diffusers)

Published:1980 Issue: Volume: Page:290-323
ISSN:
Container-title:Contributions to the Development of Gasdynamics
language:
Short-container-title:

Author:

Oswatitsch Klaus

Publisher

Vieweg+Teubner Verlag

Link

http://link.springer.com/content/pdf/10.1007/978-3-322-91082-0_18.pdf

Reference3 articles.

1. Eggink: Strömungsaufbau und Druckrückgewinn in Überschallkanälen. (Flow Structure and Pressure Recovery in Supersonic Channels.) ZWB-Forschungsbericht No. 1756.

2. F. Schubert: Zur Theorie des stationären Verdichtungsstoßes. (On the Theory of the Stationary Compression Shock.) Z.A.M.M., vol. 23, no. 3, p. 132, June 1943.

3. A. Naumann: Wirkungsgrad von Diffusoren bei hohen Unterschallgeschwindigkeiten. (Efficiency of Diffusers at High Subsonic Velocities.) ZWB-Forschungsbericht No. 1705.

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