Transonic Aerodynamic Characteristics of a Supercritical-wing Transport Model with Trailing-edge Controls
Author: Michael J. Mann
Publisher:
Published: 1977
Total Pages: 348
ISBN-13:
DOWNLOAD EBOOKThe effects of wing trailing-edge control surfaces on the static transonic aerodynamic characteristics of a transport configuration with a supercritical wing were studied. The configuration was tested with both an area-ruled fuselage and a cylindrical fuselage. The Mach number range was from 0.80 to 0.96 and the angle of attack range was from -1 deg to 12 deg. The Reynolds number was 1,580,000 based on the mean aerodynamic chord. Tabular data are presented.