Effects of leading-edge slat and trailing-edge split flap on the aerodynamic characteristics of a wing-fuselage combination having a nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92

Demele, Fred A
naca-rm-a57h19
January 12, 1958


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1958/naca-rm-a57h19.pdf