Lift Tests of a 0.1536c Thick Douglas Airfoil Section of NACA 7-Series Type Equipped with a Lateral-Control Device for Use with a Full-Span Double-Slotted Flap on the C-74 Airplane
1945-03-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - DOUGLAS - CHAR & ORDINATES - WING FLAPS, SLOTTED (DOUBLE) , LIFT COEFFICIENTS - AIRFOILS - DOUGLAS , WING FLAPS, SLOTTED - DOUBLE , AIRPLANES - RANGE, LONG , LATERAL CONTROL DEVICES , AIRFOILS - NACA 7-SERIES - CHAR & ORDINATES - WING FLAPS, SLOTTED (DOUBLE) , AILERONS, SLOT-LIP , AIRPLANES - DOUGLAS C-74 (AMER )
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1942
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