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- W1486272540 abstract "Additional tests as recommended in reference 1 were made in the 7- by 10-foot wind tunnel of the 1/8-scale model of the Brewster F2A airplane to determine the angle of attack of horizontal tail and the elevator angles required for trim with flaps down (p. 1)." @default.
- W1486272540 created "2016-06-24" @default.
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- W1486272540 date "1941-08-01" @default.
- W1486272540 modified "2023-09-27" @default.
- W1486272540 title "Additional Power-on Wind-tunnel Tests of the 1/8-scale Model of the Brewster F2A Airplane with Full-span Slotted Flaps" @default.
- W1486272540 hasPublicationYear "1941" @default.
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