Icing Induced Structural Problems
SM_ENV_1970-3083
11/16/1970
- Content
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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.
- 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.