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

Keyword Search

Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modification of aileron nose and adjacent airfoil contour

Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds

Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96

Published Year

• 1940-1949 (1)
• 1950-1959 (3)

Subject

• Trailing edges (Aerodynamics) (4) *
• Charts, diagrams, etc (3)
• Aerodynamics, Supersonic (2)
• Airplanes--Wings, Triangular (2)
• Hinge moments (Aerodynamics) (2)
• Wind tunnel testing (2)
• Aerodynamic load (1)
• Aerodynamics, Transonic (1)
• Aerofoils (1)
• Aerofoils--Testing (1)
• Ailerons (1)
• Airplanes--Control surfaces (1)
• Airplanes--Control systems--Testing (1)
• Drag (Aerodynamics) (1)
• Flaps (Airplanes) (1)
• Mach number (1)
• Trailing edge flaps (1)

Author

• Guy, Lawrence D. (2)
• Bird, J. D. (1)
• Brown, Hoyt V. (1)
• Katz, Ellis. (1)
• Morrow, John D. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

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