11th Fluid and PlasmaDynamics Conference 1978
DOI: 10.2514/6.1978-1148
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Artificial compressibility methods for numerical solutions of transonic full potential equation

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Cited by 52 publications
(23 citation statements)
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“…The FP formulation is the most efficient of the three in terms of accuracy-to-cost ratio for a wide range of inviscid transonic flow applications for real geometries. TSD is valid for thin wings at free stream Mach numbers near unity, and EU, while the least restrictive, involves the most complicated system of equations.During the last few years, many numerical calculations using FP have been presented, e.g., [19], [14], [17], and [6]. The object of our present investigation is twofold.…”
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confidence: 96%
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“…The FP formulation is the most efficient of the three in terms of accuracy-to-cost ratio for a wide range of inviscid transonic flow applications for real geometries. TSD is valid for thin wings at free stream Mach numbers near unity, and EU, while the least restrictive, involves the most complicated system of equations.During the last few years, many numerical calculations using FP have been presented, e.g., [19], [14], [17], and [6]. The object of our present investigation is twofold.…”
mentioning
confidence: 96%
“…During the last few years, many numerical calculations using FP have been presented, e.g., [19], [14], [17], and [6]. The object of our present investigation is twofold.…”
mentioning
confidence: 96%
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“…If equations (5) and (6) are written in quasi linear form, these equations will have two characteristics with slopes given by (8) The directionality of the two characteristics is determined by the sign of equation (8) which is the same as the sign of u ± c where c is the local isentropic sound speed. The directionality of the characteristics at the boundary points will be used in a later section to determine how many boundary conditions may be applied at each boundary.…”
Section: Introductionmentioning
confidence: 99%