Advanced Composite Material Applications to F-14A Structure

H Forsch

doi:10.1520/STP36900S

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

Advanced Composite Material Applications to F-14A Structure

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