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CONSTRUCTION OF OPTIMUM AIRFOIL FOR HYPERSONIC AIRCRAFT

机译:超音速飞机的最佳翼型构造

摘要

FIELD: aircraft engineering.;SUBSTANCE: proposed method comprises subjecting the aircraft airfoil to effects with application of optimisation criterion. The latter represents the relationship between the factors of lift and drag wherefrom optimum aircraft airfoil is derived to solve the problem of deviation from collision with application of numerical methods of the solution of complete equations of Navier-Stocks. Note here that rational arrangements of structural surfaces and aircraft nose shape are defined for minimum heat loads.;EFFECT: optimised deviation from collision.;8 dwg
机译:领域:所提出的方法包括应用优化准则使飞机机翼受到影响。后者代表了升力和阻力因素之间的关系,通过应用Navier-Stocks完整方程组的数值方法,得出了最佳飞机翼型来解决碰撞偏离问题。请注意,为最小热负荷定义了结构表面和飞机机头形状的合理布置;效果:最佳的碰撞偏离; 8 dwg

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