Add to ORKGThis report presents a convenient method for calculating the pitching-moment characteristics of tapered wings with sweepback and twist. The method is based on the fact that the pitching-moment characteristics of a wing may be specified by giving the value of the pitching moment at zero lift and the location of the axis about which the axis is constant. Data for calculating these characteristics are presented by curves which apply to wings having a linear distribution of twist along the span and which cover a large range of aspect ratios. The curves are given for wings having straight taper and distorted elliptical plan forms. The characteristics of wings of other shapes may be determined by interpolation
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ra...
The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from t...
This report presents a convenient method for calculating the pitching-moment characteristics of tape...
Stability derivatives have been computed for twisted wings of different plan forms that include vari...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
One of the problems connected with the sweptback wing is the difficulty of controlling the location ...
The application of aerodynamic theory for estimating the force and moments acting upon spinning airp...
A new empirical law for the prediction of the zero-lift pitching moment coefficient of trapezoidal w...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
Design curves are presented which permit rapid estimations of lift and pitching moment for given val...
This report deals with the application of the airfoil and twisted wing theory to the calculation of ...
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ra...
The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from t...
This report presents a convenient method for calculating the pitching-moment characteristics of tape...
Stability derivatives have been computed for twisted wings of different plan forms that include vari...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
One of the problems connected with the sweptback wing is the difficulty of controlling the location ...
The application of aerodynamic theory for estimating the force and moments acting upon spinning airp...
A new empirical law for the prediction of the zero-lift pitching moment coefficient of trapezoidal w...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
Design curves are presented which permit rapid estimations of lift and pitching moment for given val...
This report deals with the application of the airfoil and twisted wing theory to the calculation of ...
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ra...
The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from t...