Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators-Reference-Cited by-同舟云学术

Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators

Published:2014-06 Issue:6 Volume:52 Page:1207-1218
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Valdivia A.¹,Yuceil K. B.²,Wagner J. L.¹,Clemens N. T.¹,Dolling D. S.¹

Affiliation:

1. Center for Aeromechanics Research, The University of Texas at Austin, Austin, Texas 78712-1085

2. Department of Astronautical Engineering, Istanbul Technical University, 34469 Istanbul, Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052214

Reference49 articles.

1. CurranE. T.StullF. D. “The Utilization of Supersonic Combustion Ramjet Systems at Low Mach Numbers,” Aero Propulsion Lab. Rept. RTD-TDR-63-4097, Wright-Patterson AFB, OH, Jan. 1964.

2. Fluid Phenomena in Scramjet Combustion Systems

3. EmamiS.TrexlerC. A.AuslenderA. H.WeidnerJ. P. “Experimental Investigation of Inlet-Combustor Isolators for a Dual Mode Scramjet at a Mach Number of 4,” NASA TP-3502, May 1995.

4. Analysis of Flows in Scramjet Isolator Combined with Hypersonic Inlet

5. Effects of Hypersonic Inlet Flow Non-Uniformities on Stabilising Isolator Shock Systems

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