Probabilistic Methods to Determine Resonance Risk and Damping for Rocket Turbine Blades-Reference-Cited by-同舟云学术

Probabilistic Methods to Determine Resonance Risk and Damping for Rocket Turbine Blades

Published:2013-11 Issue:6 Volume:29 Page:1367-1373
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Brown Andrew M.¹,DeHaye Michael¹,DeLessio Steven²

Affiliation:

1. Propulsion Structural & Dynamic Analysis, NASA Marshall Space Flight Center, Huntsville, Alabama 35812

2. Jacobs, Inc., Huntsville, Alabama 35812

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34834

Reference21 articles.

1. OberkampfW. L.TrucanoT. G.HirschC. “Verification, Validation, and Predictive Capability in Computatiional Engineering and Physics,” Sandia National Lab., Rept. SAND2003-3769, Feb. 2003, p. 21.

2. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions

3. PackardM. H. “The Use of Probabilistic Methods to Evaluate the Systems Impact of Component Design Improvement on Large Turbofan Engines,” NASA CP-2002-211682, 2002.

4. BrownA. M. “Development of a Probabilistic Dynamic Synthesis Method for the Analysis of Non-Deterministic Structures,” Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta, GA, 1998.

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