スポンサーリンク
Institute of Space and Astronautical Science / Japan Aerospace Exploration Agency | 論文
- Numerical study on propagation of cylindrical detonation
- Effects of initial pressure on single spinning detonation in a square tube
- Numerical Study and Performance Prediction for Gaseous Hydrogen/Oxygen Bell Nozzle
- Mass Transfer around a Cold Cylinder with Condensation of Vapor (1st Report) : Mass Flux Decrease Due to Condensation of Vapor at Surface Temperatures from 200 to 250K
- Numerical simulation on hydrogen fuel jetting from high pressure tank
- Numerical Study and Performance Evaluation for a Pulse Detonation Engine with an Exhaust Nozzle : 1st Report : Estimation on Performance using a Detailed Reaction Model