Acoustically Induced Shock Oscillations in a Low-Boom Inlet-Reference-Cited by-同舟云学术

Acoustically Induced Shock Oscillations in a Low-Boom Inlet

Published:2016-07 Issue:7 Volume:54 Page:2134-2148
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Candon Sean¹,Loth Eric¹,Rybalko Michael²,Hirt Stefanie³

Affiliation:

1. University of Virginia, Charlottesville, Virginia 22904

2. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

3. NASA John H. Glenn Research Center, Cleveland, Ohio 44135

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054300

Reference28 articles.

1. FisherS. A.NealeM. C.BrooksA. J. “On the Sub-Critical Stability of Variable Ramp Intakes at Mach Numbers Around 2,” National Gas Turbine Establishment Rept. ARC-R/M-3711, England, U.K. Feb. 1970.

2. FerriA.NucciL. M. “The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions,” NACA Rept. RM-L50K30, 1951.

3. DaileyC. S. “Supersonic Diffuser Instability,” Ph.D. Dissertation, California Inst. of Technology, Pasadena, CA, 1954.

4. Experimental Study of Supersonic Inlet Buzz

5. Unsteadiness in shock wave boundary layer interactions with separation

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