[国立清华大学工程学]一·国立工程学报编辑部国立

【国立清华大学工程学】一 - 国立工程学报编辑部国立.pdf本期要目 1.SymmetricalConicalFlowatSupersonicSpeedby PurturbationMethod 钱偉長 1-14 2.不规则平面形之静矩,重心惯性矩及惯性之新計算法 蔡方蓝 15-30 3.用分配臀率法解算多跨锯菌形架構.金31-52 4.通對稀分子.孫貂先 53-62 5.機翼性能之简單求法 屠守鳄 63-79 6.RestrictedTorsionofThin-WalledColumnsofAir-Foil Sections.哲敏80-102 1 t.+7.WEI-ZANGCHIEN It should benoted thatboth solutions of Karman-Mooreand Busemann are based upon the linearized equation.In both solutions,no shock wave conditions have been taken into account.Itis inportant in general toknow the accuracy gained byworkingintonext few approximations,and by taking intoacWEI-ZANGCHIEN In terms of W,the pressure acting on the surface of cone can be evaluated through the expression[1].PThe conditionat thesurface ofconeis that theflow should beparallel to the cone surface.dr =tan0= dx 1+Ywhere O is the semi-angle of the cone.
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