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- W624626087 abstract "Report presenting an investigation to determine the damping-in-roll characteristics of a 42.7 degree sweptback wing using a linearly twisted wing to represent a rolling wing. Results regarding the effect of the airfoil contour, damping-in-roll coefficient, wing-tip helix angle, and theoretical results are provided." @default.
- W624626087 created "2016-06-24" @default.
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- W624626087 date "1949-08-08" @default.
- W624626087 modified "2023-09-27" @default.
- W624626087 title "Damping-in-roll characteristics of a 42.7 degree sweptback wing as determined from a wind-tunnel investigation of a twisted semispan wing" @default.
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