Accession Number : AD0780774
Title : NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E: Static Test Results.
Descriptive Note : Final rept.,
Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE TECHNOLOGY DEPT
Personal Author(s) : Libeskind,Mark ; Minecci,Joseph ; Huang,S. L. ; McQuillen,Edward J.
Report Date : 03 DEC 1973
Pagination or Media Count : 29
Abstract : A graphite-epoxy composite wing for the BQM- 34E unmanned supersonic aerial target vehicle has been successfully static tested to 100 percent design limit load at the NAVAIRDEVCEN (Naval Air Development Center). Test procedures and results are described, and comparisons between analytical predictions and recorded values are presented. Good correlation between analysis and test was observed. On the basis of this test, the composite wing is considered statically quali-fied for flight. (Author-PL)
Descriptors : *Wings, Composite materials, Epoxy resins, Graphite, Target drones, Static tests, Structural properties, Supersonic airfoils, Loads(Forces)
Subject Categories : Pilotless Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE