发明名称 |
CONSTRUCTION OF OPTIMUM AIRFOIL FOR HYPERSONIC AIRCRAFT |
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 |
申请公布号 |
RU2558498(C2) |
申请公布日期 |
2015.08.10 |
申请号 |
RU20130157078 |
申请日期 |
2013.12.24 |
申请人 |
FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "MOSKOVSKIJ GOSUDARSTVENNYJ UNIVERSITET LESA" (FGBOU VPO "MGUL") |
发明人 |
GALAKTIONOV ALEKSEJ JUR'EVICH;LIKHACHEVA EKATERINA SERGEEVNA |
分类号 |
B64F5/00;G06F17/50 |
主分类号 |
B64F5/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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