Theory and test of flow mixing for turbofan engines.-Reference-Cited by-同舟云学术

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Theory and test of flow mixing for turbofan engines.

Published:1968-11 Issue:6 Volume:5 Page:522-527
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

HARTMANN A.¹

Affiliation:

1. Dornier GmbH, Friedrichshafen, Bodensee, West Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.43978

Reference6 articles.

1. Barley, R. R. and Byrant, L. "Experimental Investigation of Jet Mixing of Two Subsonic Streams at Various Temperature, Mach Number and Diameter Ratios of Three Configurations," Memo. 12-21-58-E, NASA.

2. Viktorin, K. "Investigations of Turbulent Mixing Processes," Verein Deutscher Ingenieure-Forschungsheft, Band 12, Heft 1.

3. Axial- und Radialkompressoren

Cited by 3 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. Effect of mixing Mach number and mixing efficiency on the preliminary cycle design of mixed high-BPR turbofans;Thermal Science and Engineering Progress;2019-05

2. Mixing effectiveness test of an exhaust gas mixer in a high bypass turbofan at altitude;17th Joint Propulsion Conference;1981-07-27

3. Correlation of Turbofan Engine Thrust Performance with Comnound Nozzle Flow Theorv;Journal of Aircraft;1971-07

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