Numerical simulation of jet mixing in supersonic crossflow: Effect of jet exit geometry
T Iwasa, N Tsuboi - TRANSACTIONS OF THE JAPAN SOCIETY FOR …, 2022 - jstage.jst.go.jp
Implicit large-eddy simulation/Reynolds-averaged Navier-Stokes hybrid simulation of sheet-
like hydrogen jets in a supersonic crossflow are performed to investigate jet mixing, focusing …
like hydrogen jets in a supersonic crossflow are performed to investigate jet mixing, focusing …
Effects of a Recess on Coaxial Cryogenic Injections at Supercritical Pressure
D Muto, H Terashima, T Araki, N Tsuboi - Journal of Propulsion and …, 2022 - arc.aiaa.org
Effects of recess lengths on coaxial cryogenic jets under a supercritical pressure are
numerically studied. A hybrid large-eddy simulation/Reynolds-averaged Navier–Stokes …
numerically studied. A hybrid large-eddy simulation/Reynolds-averaged Navier–Stokes …
Combustion Characteristics of Shear Coaxial Injectors with Different Recess Lengths Under Wide Operating Conditions
C Kang, S Lee, K Ahn - International Journal of Aeronautical and Space …, 2024 - Springer
The advancement of space launch technologies necessitates engines with a broad thrust
control range. This study examines the impact of injector recess length on combustion …
control range. This study examines the impact of injector recess length on combustion …
Effects of a recess on supercritical co-flowing planar jets
D Muto, H TERASHIMA, N Tsuboi - Transactions of the Japan …, 2019 - jstage.jst.go.jp
The effects of a recess on co-flowing planar jets under supercritical pressure are numerically
studied. Two-dimensional hybrid LES/RANS simulations are performed in a wide range of …
studied. Two-dimensional hybrid LES/RANS simulations are performed in a wide range of …
[PDF][PDF] 超音速流れにおけるシート状噴流の混合と燃焼に関する数値解析
岩佐聡洋， イワサトシヒロ - 2022 - kyutech.repo.nii.ac.jp
現在, 人工衛星や探査機, 補給機を宇宙へ輸送するため, 各国で液体燃料を用いた輸送ロケットが
打ち上げられている. 液体燃料ロケットの更なる発展には, 機体やエンジンの性能だけでなく安全性 …
打ち上げられている. 液体燃料ロケットの更なる発展には, 機体やエンジンの性能だけでなく安全性 …