Method for applying deformation relations derived in NAE Laboratory Report LR-28 for wings without taper, to analysis of wings with moderate degree of taper; by way of illustration, experimental results for wing models of cellulose acetate yawed at 0,30,45, and 60 ° were used. (received 1955)
Deformation analysis of tapered swept wings
Canada. Nat Aeronautical Establishment -- Report
1953
12 pages
Report
English
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The deformation analysis of tapered swept wings
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