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

Keyword Search

Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section.Transonic-bump method

Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination

Published Year

• 1940-1949 (1)
• 1950-1959 (1)

Subject

• Charts, diagrams, etc (2)
• Aerodynamics (1)
• Airplane--Wings, Swept-back (1)
• Airplanes--Wings, Swept-back (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Rockets (Aeronautics)--Launching (1)
• Rockets (Aeronautics)--Models (1)
• Wind tunnel testing (1)

Author

• King, Thomas J. (2) *
• Alford, William J. (1)
• Myers, Boyd C. (1)
• Silvers, H. Norman. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

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