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- W1482096520 abstract "Report discussing an investigation to determine the effects of sweepback and low aspect ratio on the aerodynamic characteristics of a wing at high subsonic Mach numbers. Tests were performed at aspect ratios of 2, 3, and 5 and sweepback angles of 0, 30, and 45 degrees. Generally, sweepback and low aspect ratio were found to both delay and lessen the effects of compressibility." @default.
- W1482096520 created "2016-06-24" @default.
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- W1482096520 date "1947-06-04" @default.
- W1482096520 modified "2023-09-24" @default.
- W1482096520 title "Effects of combinations of aspect ratio and sweepback at high subsonic Mach numbers" @default.
- W1482096520 hasPublicationYear "1947" @default.
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