Accession Number : ADP003707

Title :   Sonic Fatigue Design Method for the Response of CFRP (Carbon-Fibre Reinforced Plastic) Stiffened-Skin Panels,

Corporate Author : ROHR INDUSTRIES INC CHULA VISTA CA

Personal Author(s) : Holehouse,I.

Report Date : 1984

Pagination or Media Count : 12

Abstract : This paper describes the development of a semi-empirical method to estimate the structural response of cfrp stiffened-skin panels when method suitable for practical use in the design of crfp airplane structures, utilizing the results from previous work.

Descriptors :   *Structural mechanics, *Structural response, *Aircraft panels, *Sonic fatigue, *Regression analysis, Acoustics, Loads(Forces), Equations, Confidence level

Distribution Statement : APPROVED FOR PUBLIC RELEASE