High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)
High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)
- New search for: Goethert, B.
- New search for: Goethert, B.
In the following, high-speed measurements on a swept-back wing are reported. The curves of lift, moment, and drag have been determined up to Mach numbers of M = 0.87, and they are compared to a rectangular wing. Through measurements of the total-head loss behind the wing and through schlieren pictures, an insight into the formation of the compression shock at high Mach numbers has been obtained.
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High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)
1947-03-01
Miscellaneous
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English
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High-speed measurements on swept-back wing (Sweepback Angle phi=35°)
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