Force and pressure distribution measurements on rectangular modified Mustang wing to investigate improvement of maximum lift coefficient obtained by use of nose flaps. English abstract from ZWB Untersuchungen u Mitteilungen n 3153 Sept 22 1944.
Wind-tunnel investigations on changed Mustang profile with nose flap force and pressure-distribution measurements
Nat Advisory Committee Aeronautics -- Tech Memo
1947
18 pages
Report
Englisch
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Systematic wind-tunnel measurements on laminar wing with nose flap
Engineering Index Backfile | 1947
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