Numerical Solutions of Nonsteady Two-Dimensional Transonic Flows
Keyword(s):
An alternating-direction implicit algorithm is applied to solve an improved formulation of the low-frequency, small-disturbance, two-dimensional potential equation. Linear solutions are presented for oscillating trailing edge flaps, plunging and pitching flat-plate airfoils, and compared with results obtained by a doublet-lattice-method. Nonlinear calculations for both steady and unsteady flow problems are then compared with results obtained by using the complete Euler equations. The present procedure allows one to solve complex aerodynamic problems, including flows with shock waves.
2019 ◽
Vol 136
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pp. 139-151
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2013 ◽
Vol 255
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pp. 471-485
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1980 ◽
Vol 47
(3-4)
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pp. 317-323
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1992 ◽
Vol 111
(3)
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pp. 279-293
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A note on the alternating direction implicit method for the numerical solution of heat flow problems
1957 ◽
Vol 8
(2)
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pp. 409-409
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Compact alternating direction implicit method for two-dimensional time fractional diffusion equation
2012 ◽
Vol 231
(6)
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pp. 2621-2633
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2006 ◽
Vol 54
(4)
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pp. 1207-1214
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