Experimental investigation of outflow boundary conditions used in unsteady inlet flow computations-Reference-Cited by-同舟云学术

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Experimental investigation of outflow boundary conditions used in unsteady inlet flow computations

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Freund Donald¹,Sajben Miklos¹,Freund Donald¹,Sajben Miklos¹

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-610

Reference14 articles.

1. Chung, J. and Cole, G.L."Comparison of Compressor Face Boundary Conditions for Unsteady CFD Simulations of Supersonic Inlets," AIAA paper 95-2627.

2. Mayer, W.D.and Paynter, G.C. "Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances," ATAApaper 94-0580.

3. Decher, R, Mayer, D.W.and Paynter, G.C."On Supersonic Inlet-Engine Stability," AIAA paper 94-3371.

4. Boundary conditions for unsteady supersonic inlet analyses

5. Clark, L.T."Dynamic Response Characteristics of aMixed Compression SupersonicInlet asa Part of aLarger System," AIAApaper 95-0036.

Cited by 8 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. Design of a Near-Isentropic Supersonic Inlet Using Active Control;Journal of Propulsion and Power;2005-03

2. Inlet/Compressor System Response to Short-Duration Acoustic Disturbances;Journal of Propulsion and Power;2002-07

3. Acoustic-Wave/Blade-Row Interactions Establish Boundary Conditions for Unsteady Inlet Flows;Journal of Propulsion and Power;2001-09

4. Modeling the Response from a Cascade to an Upstream Acoustic Disturbance;AIAA Journal;2000-08

5. Experiment to Support the Formulation and Validation of Compressor-Face Boundary Conditions;Journal of Propulsion and Power;2000-05

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