Analysis and testing of the Vulcain 2 LOX turbine blades for prediction of high cycle fatigue life-Reference-Cited by-同舟云学术

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

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Holmedahl K.¹

Affiliation:

1. Volvo Aero Corp., Trollhattan, Sweden

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3680

Reference4 articles.

1. S.Trollheden, B. Bergenlid, A. Aglund, A.I. Pettersson, Development ofthe Turbines fortheVulcain 2Turbopumps , AIAA 99-2342,

2. S.Andersson and S. Trollheden, AerodynamicDesign andDevelopment of atwo-stage supersonicTurbine for RocketEngines,AIAA-99-2192,

3. U.Wahlen, I Sjunnesson andP. Groth, Measurement and Prediction of Unsteady BladeLoads in a Supersonic/Transonic Turbine, AIAA-97-2755,

4. G. Csaba, ModelingMicroslipFriction Damping and its Influence on Turbine BladeVibrations, Doctoral dissertation no. 519,Linkoping University, Sweden, ISBN 91-7219-168-6

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. HCF and LCF Analysis of a Generic Full Admission Turbine Blade;Aerospace;2023-02-08

2. Flutter Free Design of Aerodynamically Unstable Supersonic Turbines;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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