A mathematical model of hybrid combustion regression is derived which rationally encompasses the chemical kinetic and gasdynamic factors. Data from Smoot and Price (AIAA J. v3 p1408 1965) are used to confirm the resulting regression rate equation.
Hybrid Rocket Combustion Regression Rate Model
1966
2 pages
Report
No indication
English
Hybrid rocket combustion regression rate model.
AIAA | 1966
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AIAA | 1992
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Online Contents | 2014
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