AIAA-2007-1339 INVESTIGATION OF HOT STREAK-TO-AIRFOIL COUNT RATIO EFFECTS IN HIGH PRESSURE STAGE OF VANELESS COUNTER-ROTATING TURBINE
AIAA-2007-1339 INVESTIGATION OF HOT STREAK-TO-AIRFOIL COUNT RATIO EFFECTS IN HIGH PRESSURE STAGE OF VANELESS COUNTER-ROTATING TURBINE
- Neue Suche nach: Qingjun, Z.
- Neue Suche nach: Huishe, W.
- Neue Suche nach: Zhao, X.
- Neue Suche nach: Xu, J.-z.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: Qingjun, Z.
- Neue Suche nach: Huishe, W.
- Neue Suche nach: Zhao, X.
- Neue Suche nach: Xu, J.-z.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
Dokumentinformationen
AIAA-2007-1339 INVESTIGATION OF HOT STREAK-TO-AIRFOIL COUNT RATIO EFFECTS IN HIGH PRESSURE STAGE OF VANELESS COUNTER-ROTATING TURBINE
18th, International symposium on air breathing engines IASBE ; 2007 ; Beijing, China
2007-01-01
215 pages
Aufsatz (Konferenz)
Englisch
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