Investigation of the Effect of Balancing Tabs on the Hinge-moment Characteristics of a Trailing-edge Flap-type Control on a Trapezoidal Wing at a Mach Number of 1.61
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Driver, Cornelius↗
Engineering topics
Driver, Cornelius
Publications and source records attributed to Driver, Cornelius.
Wind-tunnel Investigation of a Ram-jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges : Force and Moment Characteristics of Various Combinations of Components at a Mach Number of 1.6
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Sevier, John R , Jr↗
Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effect at M = 2.01 of Nacelle Shape and Position on the Aerodynamic Characteristics in Pitch of Two Wing-body Combinations with 47 Deg Sweptback Wings
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Driver, Cornelius↗
Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effects of Sweep Angle and Thickness Ratio on the Aerodynamic Characteristics in Pitch
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Driver, Cornelius↗