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- W242567206 abstract "Report presenting the results of deflection tests on the wing of a full-scale, swept-wing jet bomber in the form of structural influence coefficients relating the deflection of a system of points on the wing and concentrated loads applied on the wing spars. The procedures for determining the coefficients are included." @default.
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- W242567206 date "1954-04-22" @default.
- W242567206 modified "2023-09-27" @default.
- W242567206 title "Experimental influence coefficients for the deflection of the wing of a full-scale, swept-wing bomber" @default.
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