Low-speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-wing : Fuselage Combination at a Reynolds Number of 6.0 x 10(exp 6)
10.09.1951
Sonstige
Keine Angabe
Englisch
Investigation of double slotted flaps on swept-wing transport model
Engineering Index Backfile | 1959
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