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Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 被引量:7
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作者 GuangLi Li Kai Cui +3 位作者 YingZhou xu HaoXiang Wang Jing Yang xiangui xu 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS CSCD 2020年第5期124-126,共3页
Lift-to-drag ratio (L/D) is nearly the most important index in determining the aerodynamic performance of a hypersonic flight vehicle,because the flight distance is linearly proportional to the L/D according to Bregue... Lift-to-drag ratio (L/D) is nearly the most important index in determining the aerodynamic performance of a hypersonic flight vehicle,because the flight distance is linearly proportional to the L/D according to Breguet's equation.In general,the higher the L/D of a vehicle,the greater the flight range if the specific impulse,structural mass ratio,and flight velocity are given.Naturally,the pursuit of a high L/D for hypersonic vehicles has never ceased [1,2]. 展开更多
关键词 CONFIGURATION SHAPED PURSUIT
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