ASM Failure Analysis Case Histories: Air and Spacecraft
Analysis of a Failed UH-1N Helicopter Main Rotor Blade Grip
-
Published:2019
Abstract
Proper stress analysis during component design is imperative for accurate life and performance prediction. The total stress on a part is comprised of the applied design stress and any residual stress that may exist due to forming or machining operations. Stress-corrosion cracking may be defined as the spontaneous failure of a metal resulting from the combined effects of a corrosive environment and the effective component of tensile stress acting on the structure. However, because of the orientation dependence in aluminum, it is the residual stress occurring in the most susceptible direction that must be considered of primary importance in...
Sign in
ASM members
Member Sign InD.S. Parker, Analysis of a Failed UH-1N Helicopter Main Rotor Blade Grip, ASM Failure Analysis Case Histories: Air and Spacecraft, ASM International, 2019, https://doi.org/10.31399/asm.fach.aero.c9001510
Download citation file:
Join ASM International
Being a member of the world’s largest association of materials professionals provides the benefits and resources you need to accomplish your personal and professional goals.