Program involving design, development, test, and evaluation of boron-fiber-reinforced airframe component is described; development article is approximate half-scale representation of aircraft structural beam-column scaled to simulate thickness ratio, slenderness ratio, and stress levels of full-sized part under static design conditions; design, manufacturing, and test methods are described, and salient problem areas are discussed. (12253)
Design and development study of aircraft structural composites
Soc Aerospace Matl and Process Engrs Nat Symp
12th SAMPE National Symposium -- Advances in Structural Composites ; 1967
1967
17 pages
Conference paper
English
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