An Experimental Investigation of Supersonic Inlet Unstart-Reference-Cited by-同舟云学术

An Experimental Investigation of Supersonic Inlet Unstart

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:37th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Wagner Justin¹,Valdivia Agustin¹,Yuceil Kemal¹,Clemens Noel¹,Dolling David¹

Affiliation:

1. University of Texas at Austin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4352

Reference27 articles.

1. Fluid Phenomena in Scramjet Combustion Systems

2. 3Heiser,W.H.,andPratt,D.T.,HypersonicAirBreathingPropulsion,AIAAEducationSeries,NewYork,1993.

3. 4Emami,S.,Trexler,C.A.,Auslender,A.H.andWeidner,J.P."ExperimentalInvestigationofInlet-CombustorIsolatorsfor a Dual Mode Scramjet at aMachNumber of4," NASA TP-3502, May1995.

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

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