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Publication of JPS6442435UpublicationCriticalpatent/JPS6442435U/ja
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An investigation of real gas effects relevant to the performance of a kerosine fuelled hypersonic ramjet(Real gas effects in combustion chamber and exhaust nozzle of kerosene-fuelled hypersonic ramjet)
Jet engine thrust formulas for momentum theorem applied to the engine jet, a long cylindrical nacelle in supersonic flight, and under- and over- expanded nozzles
Farfield structure of an aircraft trailing vortex, including effects of mass injection(Wind tunnel tests to predict aircraft wake turbulence due to tip trailing vortex)
Description of a thrust vector monitoring system, an instrument capable of nondestructive probing and monitoring of exhaust flame parameters of an in-flight or ground based rocket