Investigation of the effects of leading-edge flaps on the aerodynamic characteristics in pitch at Mach numbers from 0.40 to 0.93 of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4 Page: 1 of 38
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T AERODYNAMIC CHARACTERISTICS IN PITCH AT MACH
y Kenneth P. Spreema William Alfordr.
INVESTIGATION OF TE EFFECTS OF LEADING-EDGE FLAPS ON
THE AERODYNAMIC CHARA CTERISTICS IN PITCH AT MACH
S -NUMBERS FROM 0.40 TO 0.93 OF A WING-FUSELAGE
, I CONFIGURATION WITH A 450 SWEPTBACK WING
OF ASPECT RATIO 4
tj By Kenneth P. Spreemann and William . Aford, Jr.
Langley Aeronautical Laboratory
":angley Field, Va .
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Spreemann, Kenneth P. & Alford, William J., Jr. Investigation of the effects of leading-edge flaps on the aerodynamic characteristics in pitch at Mach numbers from 0.40 to 0.93 of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4, report, August 20, 1953; (digital.library.unt.edu/ark:/67531/metadc59660/m1/1/: accessed November 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.