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- W2740523003 abstract "Euler computations have been made for simulating transonic flow over a cropped Delta wing with a deflected aileron. A 28-block multiblock grid has been generated for this configuration, and two different finite volume flow solvers have been used for the computations, one with a cell-vertex formulation, JUEL3D developed at NAL, and the other with a cell-centered approach, developed at Beijing University of Aeronautics and Astronautics, China. Results are presented for the flow past the wing with aileron deflection of 6 deg. and a free stream Mach no.=0.9, at angle of incidence of 0,1 and 3 deg. The computed results are compared with available experimental data, and viscous computations available in literature." @default.
- W2740523003 created "2017-08-08" @default.
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- W2740523003 date "1999-08-01" @default.
- W2740523003 modified "2023-09-27" @default.
- W2740523003 title "Euler Computation for a Wing with Aileron Deflection" @default.
- W2740523003 hasPublicationYear "1999" @default.
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