C 105. Derivation of loads for wing design cases. Report 7/0500/16

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AVRO Museum

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C 105. Derivation of loads for wing design cases. Report 7/0500/16

Entry/Object ID

3984

Category

Report - Technical

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report checked by D. Drane

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Date / Time Period: 7/19/56 Pages: 63 Author: Brown, D, Harley, S. K Publisher: A.V. Roe Canada Limited