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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
Capabilities for turbine engine testing at the Arnold Engineering Development Center(Arnold Engineering Development Center turbine engine testing facilities and techniques for flight conditions and environment simulation, air/fuel flow and thrust measurement, etc)