Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction

@inproceedings{Dagenhart1981AmplifiedCD,
  title={Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction},
  author={J. Ray Dagenhart},
  year={1981}
}

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An aerodynamic design method for supersonic natural laminar flow aircraft

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CITES BACKGROUND & METHODS
HIGHLY INFLUENCED

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