An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor-Reference-Cited by-同舟云学术

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An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Laurence Stuart¹,Martinez Schramm Jan¹,Karl Sebastian¹,Hannemann Klaus¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2310

Reference13 articles.

1. 1Wieting,A.R."ExploratoryStudyofTransientUnstartPhenomenainaThree-DimensionalFixed-GeometryScramjet Engine",NASA TN D-8156,March 1976.

2. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

3. Load Oscillations Caused by Unstart of Hypersonic Wind Tunnels and Engines

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