Effect of Rear Face Geometry on the Open Cavity Oscillatory Flow at M=0.9-Reference-Cited by-同舟云学术

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Effect of Rear Face Geometry on the Open Cavity Oscillatory Flow at M=0.9

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:8th AIAA Flow Control Conference
language:
Short-container-title:

Author:

Das Sudip¹,Cohen Jacob²

Affiliation:

1. Birla Institute of Technology

2. Technion--Israel Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3175

Reference42 articles.

1. 2Rossiter, J. E. “Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds,” Tech. Rep. 3438, Aeronautical Research Council Reports and Memoranda. 1964.

2. Computational and experimental investigation of cavity flowfields

3. Velocity and surface pressure measurements in an open cavity

4. Supersonic Flow over a Finite-Width Rectangular Cavity

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1. Analysis of Cavity Corner Geometry Effect on Recirculation Zone Structure;Applied Sciences;2022-06-20

2. Effect of cavity rear wall modifications on pressure fluctuations at supersonic speed;Acta Astronautica;2021-08

3. Study on Oscillation Phenomena in Morphing Cavities with Ramps of Leading Wall;Journal of Aircraft;2021-05

4. Volumetric Velocimetry of Complex Geometry Effects on Transonic Flow over Cavities;AIAA Journal;2019-05

5. Influence of Impinging Wall Ramping Modification on the Flow Field of Open Cavity at M = 2.0;Journal of Fluids Engineering;2018-03-16

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