Search U.S. government technical reports digitized or harvested by TRAIL.

Keyword Search

Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds

Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01

Published Year

• 1940-1949 (1)
• 1950-1959 (1)

Subject

• Charts, diagrams, etc (2) *
• Wind tunnel testing (2)
• Aerodynamics (1)
• Aerofoils--Testing (1)
• Airplanes--Control surfaces (1)
• Airplanes--Models--Testing (1)
• Airplanes--Wngs, Swept-back (1)
• Angle of attack (Aerodynamics) (1)
• Schlieren photography (1)
• Spoilers (Airplanes) (1)

Author

• Lord, Douglas R. (2) *
• Daley, Bernard N. (1)
• Moring, Robert. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

Search developed and maintained by the University of Washington Libraries
Copyright 2010