572 research outputs found
Aerodynamic Characteristics at a Mach Number of 4.06 of a Typical Supersonic Airplane Model Using Body and Vertical-tail Wedges to Improve Directional Stability
Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form : Longitudinal and Lateral Control Characteristics
Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form : Effects of Various Tail Arrangements on Wing-on and Wing-off Static Longitudinal and Lateral Stability Characteristics
Aerodynamic characteristics of two delta wings at Mach number 4.04 and correlations of lift and minimum-drag data for delta wings at Mach numbers from 1.62 to 6.9
Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form
Effects of Sweep and Angle of Attack on Boundary-layer Transition on Wings at Mach Number 4.04
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