Calibration of a newly developed direct-connect high-enthalpy supersonic combustion research facility
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
2. Taitech, Inc., Beavercreek, OH
3. Innovative Scientific Solutions, Inc., Dayton, OH
4. Pyrodyne, Inc., New Market, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1510
Reference11 articles.
1. 500 1.962 959 4 1000 1.962 941 4 2000 1.962 935 5 500 2.385 1154 5 1000 2.385 1130 5 2000 2.385 1108 6 500 2.787 1339 6 1000 2.787 1313 6 2000 2.787 1286 7 500 3.166 1536 7 1000 3.166 1490 7 2000 3.166 1459 P* «4 4.75 2960
2. = 500psf ' 9.62 2928 1 18.39 2915 :q =1000psf 4.84 3925 = 1500psf 9.67 3889 q =2000psf 19.57 3849 4.83 4923 6 1(T - 9.53 4877 19.35 4831 4 5 6 7 * 4.74 5972 Flight Macb Number, MQ9.34 5882 Figure 1 TestCell 22 FacilityMap 18.7 5826
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2. Supersonic Combustion Experiments with a Cavity-Based Fuel Injector;Journal of Propulsion and Power;2001-11
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