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デジタル記事
インターネットで読める全国の図書館
- 要約等An experimental study has been conducted using reflected type of shock tunnel to inve......ate the effect of shock wave impingement on supersonic combustion. In the experi......d by reflected shock wave up to total temperature of 2800 K and total pressure of 0.35 MPa. Shock heated air is ...... reservoir gas of supersonic nozzle. Hydrog......eter circular sonic nozzle into free stream of Mach 2. Flow duration is around 300 microseconds. The effects of shock wave impingement on the combustion has been studi......hree different shock waves using ramp which is located on the opposite side of the supersonic nozzle wall. The wedge angles...
- 件名Shock tunnel Supersonic combustion Shock wave SCRAM-Jet
デジタル記事
インターネットで読める全国の図書館
- 件名Shock tunnel Supersonic combustion Shock wave SCRAM-Jet
- 関連情報Memoirs of the Faculty of Engineering, K......shu University || 68(1) || p31-42 九州大学工学紀要 || 68(1) || p31-42 http://stl-www.aero.ky...
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