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- W2078616265 abstract "The results of a study directed toward compilation of a theoretical and experimental data base covering inlet/airframe and nozzle/afterbody integration are described, with the major emphasis on the evaluation of the adequacy for preliminary design purposes of the data base for afterbody/propulsion system interference effects. Prediction methods that exist for afterbody/airframe interference effects are evaluated with respect to the requirements of breadth, ease of application and accuracy that are important for preliminary design." @default.
- W2078616265 created "2016-06-24" @default.
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- W2078616265 date "1979-06-18" @default.
- W2078616265 modified "2023-09-26" @default.
- W2078616265 title "Evaluation of methods for prediction of propulsion system drag" @default.
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- W2078616265 doi "https://doi.org/10.2514/6.1979-1148" @default.
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