Test results indicate: (1) by decreasing fabric deflection between pressure ribs, span load distribution was considerably modified near center and wing moment relations were changed; and (2) minimum drag was less for idling propeller than for propeller locked in vertical position.
Flight and wind-tunnel tests of XBM-1 dive bomber
Nat Advisory Committee Aeronautics -- Tech Note
1938
18 pages
22 Supp plates, Bibliography
Report
Englisch
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Flight and wind-tunnel tests of XBM-1 dive bomber
Engineering Index Backfile | 1938
|Flight and Wind-tunnel Tests of an XBM-1 Dive Bomber
NTRS | 1938
|Engineering Index Backfile | 1943
Engineering Index Backfile | 1940
Engineering Index Backfile | 1942