29 research outputs found
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 PDFNormal force, center of pressure, and zero lift drag of several ballistic-type missiles at Mach numbers of 4.05
Get PDFEffects of Sweep and Angle of Attack on Boundary-layer Transition on Wings at Mach Number 4.04
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Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form : Longitudinal and Lateral Control Characteristics
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Aerodynamic characteristics of low-aspect-ratio wings at high supersonic Mach numbers
Get PDFThis paper presents some recently obtained data on the aerodynamic characteristics of low-aspect-ratio wings at supersonic Mach numbers of 4.04 and 6.9 and discusses some new methods of predicting the lift and drag of such wings. Data on lifting wings in the Mach number range above 2.5 are not plentiful and most of the available data may be found in NACA RM L51D17, NACA RM L51D30, NACA RM L52D15a, NACA RM L52K19, NACA RM L53D03, and NACA RM L53D30
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
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
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