4,306 research outputs found
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
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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
Get PDFExploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form : Longitudinal and Lateral Control Characteristics
Get PDFStatic 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
Get PDFAerodynamic 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
Get PDFEffects of Sweep and Angle of Attack on Boundary-layer Transition on Wings at Mach Number 4.04
Get PDFNormal force, center of pressure, and zero lift drag of several ballistic-type missiles at Mach numbers of 4.05
Get PDFLongitudinal and Lateral Aerodynamic Characteristics at Combined Angles of Attack and Sideslip of a Generalized Missile Model Having a Rectangular Wing at a Mach Number of 4.08
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