Author: Charles D. HarrisPublisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Wind-tunnel Investigation of Effects of Trailing-edge Geometry on a NASA Supercritical Airfoil Section
Author: Charles D. HarrisTransonic Aerodynamic Characteristics of a Supercritical-wing Transport Model with Trailing-edge Controls
Author: Michael J. MannPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 348
Book Description
The 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.
NASA Technical Memorandum
Author: Scientific and Technical Aerospace Reports
Author: NASA Technical Paper
Author: NASA SP.
Author: Government Reports Annual Index
Author: Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1654
Book Description
Low-speed Aerodynamic Characteristics of a 9.3-percent-thick Supercritical Airfoil Section
Author: NASA Scientific and Technical Publications
Author: NASA Supercritical Airfoils
Author: Charles D. HarrisPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80
Book Description