A method using a transonic small disturbance code with successive line over-relaxation is described for treating wing/fuselage configurations with a nacelle/pylon/powered jet. Examples illustrating its use for the NASA transport research model are given. Reasonable test/theory comparisons were obtained.
Transonic Perturbation Analysis of Wing-Fuselage-Nacelle-Pylon Configurations with Powered Jet Exhausts
1982
67 pages
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Englisch