文件名称:w12sc3
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W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel
singularity distributions, based on the USSAERO program by Woodward. W12SC3
combines source and vortex panel singularity distributions forcalculating the linear
theory estimate of the configuration aerodynamics. The user can specify Woodward II
calculations for arbitrary body models or Woodward I calculations for an interference
shell that approximates actual body shape. The Carlson correction for supersonic linear
theory wing calculations is applied at wing control points. If desired, COREL will
produce conical panel pressure data for further processing by W12SC3
singularity distributions, based on the USSAERO program by Woodward. W12SC3
combines source and vortex panel singularity distributions forcalculating the linear
theory estimate of the configuration aerodynamics. The user can specify Woodward II
calculations for arbitrary body models or Woodward I calculations for an interference
shell that approximates actual body shape. The Carlson correction for supersonic linear
theory wing calculations is applied at wing control points. If desired, COREL will
produce conical panel pressure data for further processing by W12SC3
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下载文件列表
case1.inp
case1.out
files.cmn
head.cmn
input.txt
lar13239.txt
option.cmn
readme.txt
shell.cmn
w.f90
w12sc3.f90