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