Evaluation of methods for prediction of propulsion system drag
Evaluation of methods for prediction of propulsion system drag
- New search for: Kuhn, G. D.
- New search for: Mcmillan, O. J.
- New search for: Perkins, S. C., Jr.
- New search for: Perkins, E. W.
- New search for: Kuhn, G. D.
- New search for: Mcmillan, O. J.
- New search for: Perkins, S. C., Jr.
- New search for: Perkins, E. W.
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.
Document information
Evaluation of methods for prediction of propulsion system drag
AIAA, SAE, and ASME, Joint Propulsion Conference ; 1979 ; Las Vegas, NV
1979-06-01
Conference paper
No indication
English
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