Calculations of steady-state temperatures, and of temperature, mass, and trajectory histories of droplets in h-p and high-temperature environments were made to determine under what conditions critical point is reached by vaporizing drops; liquid heptane and liquid oxygen propellants were studied; boundary conditions for calculations were representative of those occurring in high-intensity combustion fields that exist in rocket engines; total gas pressures up to 2000 psi were investigated; results are presented graphically; significance to combustor design and to combustion-instability mechanisms is shown.
Calculated temperature histories of vaporizing droplets to critical point
AIAA J
AIAA Journal ; 1 , n 12
1963
7 pages
Article (Journal)
English
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Experimental and calculated histories of vaporizing fuel drops
TIBKAT | 1957
|Experimental and calculated temperature and mass histories of vaporizing fuel drops
Engineering Index Backfile | 1956
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