Investigation in the Langley 19-Foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps
1948-05-01
Sonstige
Keine Angabe
Englisch
WING FLAPS, SLOTTED - DOUBLE , AIRFOILS - CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS , AIRFOILS-NACA 64-210-CHAR , MOMENTS & ORDINAGES WING FLAPS , AIRFOILS-NACA 65-210-CHAR , MOMENTS & ORDINATES WING FLAPS , WING FLAPS, SLOTTED , WING FLAPS, SPLIT , WIND TUNNEL TESTS - NACA - PRESSURE (19') , INTERFERENC E- WINGS & FUSELAGES
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1948
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