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Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01

Published Year

• 1950-1959 (1)

Subject

• Airplanes--Tail surfaces (1)
• Airplanes--Wings, Swept-back (1)
• Charts, diagrams, etc (1)
• Mach number (1) *
• Pitching (Aerodynamics) (1)
• Stability of airplanes, Lateral (1)
• Wind tunnel testing (1)

Author

• Robinson, Ross B. (1) *
• Spearman, M. Leroy. (1)

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