Application of boron laminates in wing extension and pressurized fuel tank for F-111B aircraft; incorporation of boron-epoxy face sheets and full depth honeycomb core is principle method of construction; discussion of material testing method, design of wing extension and configuration of pressurized fuel tank, fabrication techniques and inspection procedures.
Boron wing extension for F-111B aircraft
SPE -- Annual Tech Conference
26th Annual Technical Conference of SPE ; 1968 Plastics
1968
10 pages
Conference paper
English
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