Technical Notes: Static and Fatigue Post-Buckled Behavior of Composite Shear Panels in the ACAP Design

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.29, Iss.2, 1984-04, pp. : 61-64

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Damage Tolerance of Composite Shear Panels

By Llorente Steven

Journal of the American Helicopter Society, Vol. 34, Iss. 2, 1989-04 ,pp. : 43-51

AHS International

Access to resources Recommend Favorite

Static Test Techniques for Composite Airframe Structures Developed on the U.S. Army/Sikorsky ACAP

By Kearney Hugh L. Good Dan

Journal of the American Helicopter Society, Vol. 30, Iss. 3, 1985-07 ,pp. : 43-52

AHS International

Access to resources Recommend Favorite

Effect of Moisture on Static and Fatigue Behavior of Aramid Composites

By Roylance Margaret E. Houghton William W.

Journal of the American Helicopter Society, Vol. 28, Iss. 4, 1983-10 ,pp. : 3-7

AHS International

Access to resources Recommend Favorite

Design of fiber metal laminate shear panels for ultra-high capacity aircraft

By Wittenberg T.C. van Baten T.J. de Boer A.

Aircraft Design, Vol. 4, Iss. 2, 2001-06 ,pp. : 99-113

Elsevier

Access to resources Recommend Favorite

Technical Notes: Analytical Failure Prediction of Bolted Connections in Composite Shafts

By Furnes Kenneth M. Goetschel Daniel B.

Journal of the American Helicopter Society, Vol. 34, Iss. 3, 1989-07 ,pp. : 75-79

AHS International

Access to resources Recommend Favorite