Division of Intergrated Engineering, Graduate School of Science and Engineering, Teikyo University
Division of Intergrated Engineering, Graduate School of Science and Engineering, Teikyo University
School of Science and Engineering, Teikyo University
43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8, 2011. Waseda University, International Conference Center), Tokyo Japan
抄録（英）
For accomplishment of the future space plane, it is necessary to reduce both of aerodynamic drag and heating in the ascent flight especially reduction of aerodynamic drag is focused in this study. For the purpopose of such requirement, the concept of Directed Energy Air Spike (DEAS), which makes a virtual spike by applying a heat source in front of the vehicle with use of high power laser, is applied. The experiment with aerodynamics force measurement and flow visualization using a hypersonic wind tunnel of Mach 7 of Graduate School of the Frontier Science the University of Tokyo is conducted to study the effect of reduction of aerodynamic drag by DEAS, which aims to compare the results of the above mentioned effects by DEAS with actual aerospike.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
仮想エアロスパイクに関する極超音速風洞実験
65207042.pdf
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