Analysis and testing of the Vulcain 2 LOX turbine blades for prediction of high cycle fatigue life

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Holmedahl, K ^a  

^a VOLVO AERO CORPORATION   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; LIQUEFIED GASES; PROPULSION; TURBINES; TURBOMACHINE BLADES;

ANALYSIS AND TESTING; DESIGN APPROACHES; HIGH CYCLE FATIGUE; LIFE PREDICTIONS; PRESSURE RATIO; SHROUDED BLADES; SUBCRITICAL SPEED; TURBINE BLADE;

FATIGUE OF MATERIALS;

EID: 84896457689     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. S. Trollheden, B. Bergenlid, A. Aglund, A.I. Pettersson, Development of the Turbines for the Vulcain 2. Turbopumps, AIAA 99-2342
2. S. Andersson and S. Trollheden, Aerodynamic Design and Development of a two-stage supersonic Turbine for Rocket Engines, AIAA-99-2192,
3. U. Wahlen, I Sjunnesson and P. Groth, Measurement and Prediction of Unsteady Blade Loads in a Supersonic/Transonic Turbine, AIAA-97-2755,
4. G. Csaba, Modeling Microslip Friction Damping and its Influence on Turbine Blade Vibrations, Doctoral dissertation no. 519, Linkoping University, Sweden, ISBN 91-7219-168-6