29th Aerospace Sciences Meeting 1991 Help me understand this report
Techniques for accurate, efficient computation of unsteady transonicflow
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1992
1992
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“…The method solves a discretized form of are described by Weatherill and Ehlers [161] and Shieh, Schoen, the equation using an ADI splitting technique. Unsteady generand Fang [143]. In Reference [161] the transonic small disturalized airforces are computed for a number of normal modes for bance equation is split into a steady and an unsteady flow corna swept, high-aspect-ratio transport-type wing.…”
Section: Tcrt= Ncvnsqcvngpr (25)mentioning
confidence: 99%
“…The method solves a discretized form of are described by Weatherill and Ehlers [161] and Shieh, Schoen, the equation using an ADI splitting technique. Unsteady generand Fang [143]. In Reference [161] the transonic small disturalized airforces are computed for a number of normal modes for bance equation is split into a steady and an unsteady flow corna swept, high-aspect-ratio transport-type wing.…”
Section: Tcrt= Ncvnsqcvngpr (25)mentioning
confidence: 99%
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