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

Keyword Search

Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4

Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

Published Year

• 1950-1959 (2)

Subject

• Charts, diagrams, etc (2) *
• Airplanes--Models--Testing (1)
• Airplanes--Models--Wings (1)
• Airplanes--Wings, Swept-back (1)
• Cone--Aerodynamics (1)
• Cylinders--Aerodynamics (1)
• Drag (Aerodynamics) (1)
• Flaps (Airplanes) (1)
• Leading edges (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Rockets (Aeronautics) (1)
• Stability of airplanes, Longitudinal (1)

Author

• Knechtel, Earl D. (2) *
• Andrea, Arvid N. (1)
• Lee, George. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

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