Sphere Release from a Rectangular Cavity at Mach 2.22 Freestream Conditions-Reference-Cited by-同舟云学术

Sphere Release from a Rectangular Cavity at Mach 2.22 Freestream Conditions

Published:2016-05 Issue:3 Volume:53 Page:822-829
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Merrick Justin D.¹,Reeder Mark F.¹

Affiliation:

1. U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033636

Reference7 articles.

1. DixR. E.BauerR. C. “Experimental and Theoretical Study of Cavity Acoustics,” Sverdrup Technology, Arnold Engineering Development Center TR-99-4, Arnold AFB, TN, May 2000.

2. Scaled-Drop-Tests: WYSIWYG or Not?

3. Dynamic Store Release of Ice Models from a Cavity into Mach 2.9 Flow

4. MerrickJ. “Influence of Mach Number and Dynamic Pressure on Cavity Tones and Freedrop Trajectories,” M.S. Thesis, Air Force Inst. of Technology, Dept. of Aeronautics and Astronautics, Wright–Patterson AFB, OH, March 2014.

5. NicholsR. H.BuningP. G., User’s Manual for OVERFLOW 2.1, 2nd ed., NASA, Aug. 2008, pp. 12–96.

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