Presentation Information
[CH-1-01]Numerical simulations on aerodynamic heating and flow characteristics of hypersonic Apollo-shaped capsule induced by boundary layer trip
*Kento Inokuma1, Aiko Yakeno1, Flavien Colusso1, Shuto Yatsuyanagi2, Hideyuki Tanno2 (1. Institute of Fluid Science, Tohoku University (Japan), 2. Kakuda Space Center, Japan Aerospace Exploration Agency (Japan))
Comment
To browse or post comments, you must log in.Log in