Reviewing of photographic technique for determining temperatures in luminous rocket exhaust gases; recent refinements in reduction and analysis of film records; values of temperatures measured at nozzle exit of small rocket motor are compared with theoretical values based on measurement of pressure in chamber, propellant mixture ratio, and dimensions of motor; applicability to studies of expansion process in rocket nozzles. (see also Aircraft Eng v 31 n 363 May 1959 p 144-6)
Photographic technique for measuring temperatures in luminous rocket exhaust flames
Optical Soc America -- J
Optical Society of America -- Journal ; 48 , n 10
1958
5 pages
Aufsatz (Zeitschrift)
Englisch
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Photographic technique for measuring temperatures in luminous rocket exhaust flames
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