[A-3] Air-breathing Engine 2

[2022-a-12] Experimental Investigation on the Effect of the Intake Throat Height on the Buzz Characteristics in the Ramjet Engine for High-Mach Integrated Control Experiment (HIMICO)

*Manami Fujii¹, Yuki Fujimori¹, Yusuke Hoshiya¹, Yuki Kuwabara¹, Rintaro Tanaka¹, Tetsuya Sato¹, Hidemi Takahashi², Hideyuki Taguchi³ (1. Department of Applied Mechanics and Aerospace Engineering, Waseda University, 2. Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, 3. Research and Development Directorate, Japan Aerospace Exploration Agency)

Keywords:Supersonic air intake, Wind tunnel test, Buzz, Throat height