Purpose of paper is to consolidate available theoretical and experimental data for applicable drag and heat-transfer coefficients to provide empirical relationships useful for wide range of rocket nozzle conditions; some results presented show effect of these corrections on typical calculations of particle velocities and temperatures in rocket nozzles; inertial and compressibility effects dominate for large particles and high chamber pressures, causing thermal and velocity lags to be less than those predicted under Stokes flow assumption.
Particle drag and heat transfer in rocket nozzles
AIAA J
AIAA Journal ; 2 , n 11
1964
5 pages
Aufsatz (Zeitschrift)
Englisch
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