SYMPOSIA PAPER Published: 01 June 1979
STP36900S

Advanced Composite Material Applications to F-14A Structure

Source

This paper presents a review of the advanced composite material applications to the F-14 aircraft. These composite applications include the boron/epoxy horizontal stabilizer, and the hybrid advanced composite over-wing fairing and main landing gear door.

A brief design review of each of these components is presented together with the program payoffs. A summary of composite horizontal stabilizer production and service experience also is presented and compared to typical metal aircraft service data.

Author Information

Forsch, H
Grumman Aerospace Corporation, Bethpage, N. Y.
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Details
Developed by Committee: D30
Pages: 30–39
DOI: 10.1520/STP36900S
ISBN-EB: 978-0-8031-4743-0
ISBN-13: 978-0-8031-4495-8