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- W66026724 abstract "Publisher Summary This chapter discusses various approximate methods for calculating three-dimensional boundary layer flow on wings. The boundary layer may be considered known if either the spanwise equation or the crossflow equation is solved. With digital computers becoming more commonplace in industry and the universities today, it is a waste of time to try to evolve approximate methods for the solution of differential equations. In cases where a suction distribution needs to be determined, it is a great help to be able to put into the computer a distribution of the form required as a first approximation to be amended in the light of subsequent knowledge. For such a process, a quick approximate method is obviously desirable." @default.
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- W66026724 date "1961-01-01" @default.
- W66026724 modified "2023-09-27" @default.
- W66026724 title "APPROXIMATE METHODS FOR CALCULATING THREE-DIMENSIONAL BOUNDARY LAYER FLOW ON WINGS" @default.
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- W66026724 doi "https://doi.org/10.1016/b978-1-4832-1323-1.50010-5" @default.
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