The General Problems in Vibration of Aircraft Powerplant Components

670237

02/01/1967

Event
3rd Annual Business Aircraft Conference (1967)
Authors Abstract
Content
Some of the more general types of dynamic vibration that exist in aircraft, particularly the powerplant components, are reviewed for reciprocating and turbine engines as well as helicopter and unconventional drive systems. The responsiveness of various components to the source of excitation, resulting in either resonant or nonresonant (forced) vibration, is discussed. The importance of evaluating the fatigue life of a component at varying load conditions, both in the laboratory and field, is stressed.
Meta TagsDetails
DOI
https://doi.org/10.4271/670237
Pages
10
Citation
Critchlow, E., "The General Problems in Vibration of Aircraft Powerplant Components," SAE Technical Paper 670237, 1967, https://doi.org/10.4271/670237.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670237
Content Type
Technical Paper
Language
English