Aeroengine turbine blade containment tests using high-speed rotor spin testing facility-Reference-Cited by-同舟云学术

Aeroengine turbine blade containment tests using high-speed rotor spin testing facility

Published:2006-09 Issue:6 Volume:10 Page:501-508
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xuan Hai-jun,Wu Rong-ren

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. High cycle fatigue failure in aircraft gas turbines: an industry perspective;Cowles;International Journal of Fracture,1996

2. Assessment of current turbine engine high cycle fatigue test methods;Nichol;ASME Journal of Engineering for Gas Turbines and Power,2003

3. Federal Aviation Administration (United States), Federal aviation regulation part 33, section 33.94-blade containment and rotor unbalance tests, 1984

4. Federal Aviation Administration (United States), Advisory circular: turbine engine rotor blade containment/durability, 1990

5. Ministry of Defense (United Kingdom), Defense standard 00-971-General specification for aircraft gas turbine engines, 1987

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