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Lift Characteristics of Asymmetric Exhaust Nozzles at HighFlight Speeds
Published online by Cambridge University Press: 04 July 2016
Summary
If a supersonic nozzle is designed for less than complete expansion of the flow, some lift force can be produced without downwards deflection of the nozzle. A theoretical analysis has been made, by the method of characteristics, for a two-dimensional nozzle consisting of an upper wedge and lower parallel shroud. General trends of lift performance with the main variables have been obtained.
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- Copyright © Royal Aeronautical Society 1966
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