Parametric Study of the Generation of Shocks in Near-Critical Turbofan Nozzles-Reference-Cited by-同舟云学术

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Parametric Study of the Generation of Shocks in Near-Critical Turbofan Nozzles

Published:2008-05-05 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
language:
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Author:

Kube-McDowell Matthew¹,Lyrintzis Anastasios¹,Blaisdell Gregory¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2984

Reference14 articles.

1. A Contribution to the Understanding and Prediction of Jet Noise Generation in Forced Mixers

2. A contribution to the understanding and prediction of jet noise generation in forced mixers: Part II Flight Effects

Cited by 1 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. An Overview of the NPARC Alliance's Wind-US Flow Solver;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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