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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