Report presents combined analytical and experimental approach to investigation of external aerodynamic performance of supersonic airplane-nozzle systems at subsonic speeds; experimental techniques are described which can minimize model scaling uncertainties in wind-tunnel tests; analysis method for successfully predicting drag on axisymmetric bodies at subsonic speeds combines axisymmetric potential flowfield predictions with laminar and turbulent boundary-layer computation procedures; results for certain applications are compared with experiment, and application of analysis to design of asymmetric models is demonstrated.
Subsonic aerodynamic performance of nozzle installations in supersonic airplanes
J Aircraft
Journal of Aircraft ; 5 , n 3
1968
6 pages
Article (Journal)
English
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Scaled Subsonic/Supersonic Airplanes - A Historical Perspective
British Library Conference Proceedings | 2012
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