Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric, Scramjet Combustor Flowpaths
Author:
Affiliation:
1. Air Force Research Laboratory
2. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2311
Reference11 articles.
1. Smith, S.,Gruber,M.,Steiner,R.,Collatz,M.,andMathur,T.DevelopmentandCalibrationofanAxisymmetric Direct-ConnectSupersonic CombustionFlowpath,‖ AIAAPaper 2009-5035, August2009.
2. Smith, S., Gruber, M., Mathur, T., Ryman, R., Diemer, J., and Tam, C.J.Development of a Rotating Probe Systemfor Supersonic CombustionExperiments,‖ AIAAPaper 2009-5034, August2009.
3. Gruber, M., Carter, C., Ryan, M., Rieker, G. B., Jeffries, J. B., Hanson, R. K., Liu, J., and Mathur, T.Laser-Based Measurements of OH, Temperature, and Water Vapor Concentration in a Hydrocarbon-Fueled Scramjet,‖ AIAAPaper 2008-5070,July2008.
4. Hiers, R. and Pruitt, D. "Determination of Thrust from Pitot Pressure Measurements," AIAA Paper 2001-3314, July2001.
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