Flightworthy Graphite Fiber Reinforced Composite Aircraft Primary Structural Assemblies. Volume I. Tasks 1 Through 5.
Abstract
This report presents a detailed description of the flightworthy graphite fiber reinforced composite aircraft primary structural assemblies program. The following tasks were completed: Component selection and preliminary design; materials development; test and quality control procedures development; design allowables and criteria; design allowables testing; and analysis procedure assessment and definition. Demonstration items selected were the F-5A supersonic fighter main landing gear strut door, speed brake, wing leading edge flap, wing trailing edge flap, horizontal stabilizer, and vertical stabilizer main spar. (P.S.-PL)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1972
- Accession Number
- AD0894723
Entities
People
- A. Scow
- D. Wilhem
- J. Wada
- R. D. Hayes
- R. Verette