Optical Measurements at the Combustor Exit of the HIFiRE 2 Ground Test Engine-Reference-Cited by-同舟云学术

Optical Measurements at the Combustor Exit of the HIFiRE 2 Ground Test Engine

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Brown Michael¹,Herring Gregory²,Cabell Karen²,Hass Neal²,Barhorst Todd¹,Gruber Mark¹

Affiliation:

1. Air Force Research Laboratory

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-857

Reference11 articles.

1. Jackson, K. R., Gruber, M., and Buccellato, S. "HIFiREFlight2 Overview and StatusUpdate2011,"AIAAPaper 2011-2202,2011.

2. Sappey, A., Sutherland, L., Owenby, D., VanHoudt,P., Hannam, J., Zhao, Q.,McCormick, P.,Masterson,P.,Estes, M., Williams, S., andBarhorst,T. "Flight-ReadyTDLAS CombustionSensor for Hypersonics,"AIAAPaper 2009-7234,2009.

3. Cabell, K., Hass, N.,Storch, A., and Gruber,M. "HIFiRE Direct-Connect Rig(HDCR)PhaseI Scramjet Test Results from theNASALangleyArc-Heated Scramjet Test Facility," AIAAPaper 2011-2248,2011.

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