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Effects of Nozzle Exit Geometry and Pressure Ratio on Plume Shape for NozzlesExhausting into Quiescent Air

机译:喷嘴出口几何和压力比对排气静止喷嘴羽流形状的影响

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摘要

The effects of varying the exit geometry on the plume shapes of supersonicnozzles exhausting into quiescent air at several exit-to-ambient pressure ratios are given. Four nozzles having circular throat sections and circular, elliptical and oval exit cross sections were tested and the exit plume shapes are compared at the same exit-to-ambient pressure ratios. The resulting mass flows were calculated and are also presented.

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