1,059 research outputs found
Stability Characteristics at Low Speed of a Variable-sweep Airplane Model Having a Partially Cambered Wing with Several Chord-extension Configurations
The Effect of Negative Dihedral, Tip Droop, and Wing-tip Shape on the Low-speed Aerodynamic Characteristics of a Complete Model Having a 45 Degrees Sweptback Wing
An investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing. Longitudinal and lateral stability characteristics were obtained for the model with and without tail surfaces
Wind-tunnel investigation at high subsonic speeds of the static longitudinal stability characteristics of a complete model having cropped-delta,swept, and unswept wings and several horizontal-tail heights
Wind-tunnel investigation at high subsonic speeds of the stability characteristics of a complete model having sweptback-,M-,W-,and cranked-wing plan forms and several horizontal-tail locations
Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section : transonic-bump method
Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic-bumb Method
Stability and control characteristics at low speed of a 1/4-scale Bell X-5 airplane model : lateral and directional stability and control
Investigation of the low-speed aerodynamic characteristics of a variable-sweep airplane model with a wing having partial-span cambered-leading-edge modifications
Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35 degree sweptback wings
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