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- W166290307 abstract "It is well-known that boundary-layer theory cannot be applied to the prediction of the complete flow field past an aircraft configuration, because the boundary-layer approach is not valid, for instance, for the flow along wing-fuselage junctions and along wing tips (see Fig. 6.1). The boundary-layer on portions of the aircraft, such as on wings or fuselages, can, however, be predicted quite well as long as the flow remains attached to the body surface." @default.
- W166290307 created "2016-06-24" @default.
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- W166290307 date "1981-01-01" @default.
- W166290307 modified "2023-09-27" @default.
- W166290307 title "Initial Conditions for the Prediction of Boundary Layers on Wings and Fuselages" @default.
- W166290307 doi "https://doi.org/10.1007/978-3-663-05276-0_6" @default.
- W166290307 hasPublicationYear "1981" @default.
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