The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
The University of Tokyo
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
Japan Atomic Energy Agency (JAEA)
45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan
抄録（英）
The reed-valve air-breathing system was developed to improve air-breathing performance of the microwave rocket. Air-breathing performance test was conducted using a gyrotron. Pressure history in the thruster was measured and plateau pressure was evaluated. Air-flow through the reed valve was estimated by using CFD model assuming Bernoulli-Euler beam as the reed valve. As a result, normalized plateau pressure and normalized plateau time under multi-pulse operation were increased at all repetitive-pulse frequency up to 200 Hz.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
リード弁式吸気機構によるマイクロ波ロケットの推力性能改善
62268005.pdf
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