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

Keyword Search

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method

The rolling moment due to sideslip of swept wings at subsonic and transonic speeds

Published Year

• 1940-1949 (1)
• 1950-1959 (1)

Subject

• Airplanes--Wings, Swept-back (2)
• Charts, diagrams, etc (2) *
• Wind tunnel testing (2)
• Aerodynamics (1)
• Aerofoils--Testing (1)
• Airplanes--Dihedral wings (1)
• Airplanes--Wings, Triangular (1)
• Aspect ratio (Aerofoils) (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Mathematics (1)
• Pitching (Aerodynamics) (1)
• Rolling (Aerodynamics) (1)

Author

• Sleeman, William C. (2) *
• Becht, Robert E. (1)
• Polhamus, Edward C. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

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