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Dynamic stress calculations for two airplanes in various gusts

Investigation of the dynamic response of airplane wings to gusts

Calculations of the Dynamic Stress of Several Airplane Wings in Various Gusts

Tests of a 45 degree sweptback-wing model in the Langley gust tunnel

Gust-Tunnel Investigation of a Delta-Wing Model With the Leading Edge Swept Back 60 Degrees

Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region


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