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Aerodynamic characteristics with fixed and free transition of a modified delta wing in combination with fuselage at high subsonic speeds

Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-Chord Lines Swept Back 45 Degrees, and NACA 63(Sub 1)a012 Airfoil Sections: Transonic-Bump Method

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

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations

Subsonic wind-tunnel investigation of the effect of fuselage afterbody on directional stability of wing-fuselage combinations at high angles of attack

Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing

Published Year

• 1950-1959 (6) *

Subject

• Wind tunnel testing (3)
• Charts, diagrams, etc (2)
• Aerodynamics (1)
• Airplanes--Design and construction (1)
• Airplanes--Dihedral wings (1)
• Airplanes--Fuselage (1)
• Airplanes--Models--Testing (1)
• Airplanes--Tail surfaces (1)
• Airplanes--Wings, Swept-back (1)
• Airplanes--Wings, Triangular (1)
• Aspect ratio (Aerofoils) (1)
• Loads (Mechanics) (1)
• Mathematics (1)
• Pitching (Aerodynamics)--Measurement (1)
• Rolling (Aerodynamics) (1)
• Stability of airplanes, Lateral (1)
• Stability of airplanes, Longitudinal (1)

Author

• Polhamus, Edward C. (6) *
• Sleeman, William C. (1)
• Spreemann, Kenneth P. (1)

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