Investigation of Supersonic Flow Separation in Nozzles-Reference-Cited by-同舟云学术

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Investigation of Supersonic Flow Separation in Nozzles

Published:1959-12 Issue:3 Volume:1 Page:267-279
ISSN:0022-2542
Container-title:Journal of Mechanical Engineering Science
language:en
Short-container-title:Journal of Mechanical Engineering Science

Author:

Fraser R. P.¹,Eisenklam Paul¹,Wilkie D.¹²

Affiliation:

1. High Speed Fluid Kinetics Laboratory, Department of Chemical Engineering, Imperial College of Science and Technology, London, S.W.7.

2. Now at the Development and Engineering Group U.K. Atomic Energy Authority, Windscale Works, Seascale, Cumberland.

Publisher

SAGE Publications

Subject

General Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/JMES_JOUR_1959_001_031_02

Reference10 articles.

1. Efficiency of Supersonic Nozzles for Rockets and Some Unusual Designs

2. A Review of the Performance of Exhaust Systems for Gas-Turbine Aero-Engines

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Flow Separation in Rectangular Over-Expanded Supersonic Nozzles;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

2. Investigation on onset of shock-induced separation;Shock Waves;1996-11

3. Viscous slipstream flow downstream of a centerline Mach reflection;AIAA Journal;1971-10

4. Characteristics of Separated Flows;Separation of Flow;1970

5. Compressible Flow Separation;Separation of Flow;1970

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