To study feasibility of carrying out repair of light weight aircraft skin panels using composite material graft instead of conventional metal stiffeners

By: Qais Waleed Alqaisi, 2nd LT 405160 71 ECPublisher: Risalpur NUST Risalpur 2011Description: v, 35p. Babar Saeed, Wg CdrDDC classification: PR 168
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