Icing Induced Structural Problems

SM_ENV_1970-3083

11/16/1970

Authors
Abstract
Content

Of major concern when helicopters are operated in icing conditions is the structural damage that may result as a secondary effect of the icing of the rotor blades and other components. This paper reviews these problem areas and urges greater attention to them at an early stage of a helicopter's design.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_ENV_1970-3083
Citation
Stallabrass, J. and Price, R., "Icing Induced Structural Problems," Environmental Effects on VTOL Designs - Arlington, Texas 1970, Arlington, Texas, November 16, 1970, https://doi.org/10.4050/SM_ENV_1970-3083.
Additional Details
Publisher
Published
11/16/1970
Product Code
SM_ENV_1970-3083
Content Type
Technical Paper
Language
English