Add to ORKGLift dominated pointed aircraft configurations are considered in the transonic range. These are treated as lifting wings of zero thickness with an aspect ratio of order one. An inner expansion which starts as Jones' theory is matched to a nonlinear outer transonic theory as in Barnwell's earlier work. Expressions for the wave drag due to the equivalent body are derived. Some examples of numerical calculations for different configurations are presented
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
The transonic aerodynamic characteristics of wings of finite span are discussed from the point of vi...
Induced drag is commonly regarded as the undesired side effect of the lift generation in finite aspe...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calcula...
An analytical solution was obtained for the perturbation velocity potential for transonic flow about...
The three-dimensional problem of transonic flow about lifting wing-body configurations is reduced to...
Wave drag and shock induced boundary layer separation are important issues of flows around transonic...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
The point-source-distribution method of calculating the aerodynamic coefficients of thin wings at su...
A vorticity-based exact theory for the analysis of the aerodynamic force is here applied to three-di...
An analytical approach is presented to account for some of the nonlinear characteristics of the tran...
This paper presents the wave-drag characteristics of an over-the-wing nacelle con guration. The ow...
On a typical transsonic transport-type aircraft, wave drag is only a minor component of the total dr...
A theoretical study is described of the aerodynamic characteristics at small angle of attack of a th...
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
The transonic aerodynamic characteristics of wings of finite span are discussed from the point of vi...
Induced drag is commonly regarded as the undesired side effect of the lift generation in finite aspe...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calcula...
An analytical solution was obtained for the perturbation velocity potential for transonic flow about...
The three-dimensional problem of transonic flow about lifting wing-body configurations is reduced to...
Wave drag and shock induced boundary layer separation are important issues of flows around transonic...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
The point-source-distribution method of calculating the aerodynamic coefficients of thin wings at su...
A vorticity-based exact theory for the analysis of the aerodynamic force is here applied to three-di...
An analytical approach is presented to account for some of the nonlinear characteristics of the tran...
This paper presents the wave-drag characteristics of an over-the-wing nacelle con guration. The ow...
On a typical transsonic transport-type aircraft, wave drag is only a minor component of the total dr...
A theoretical study is described of the aerodynamic characteristics at small angle of attack of a th...
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
The transonic aerodynamic characteristics of wings of finite span are discussed from the point of vi...
Induced drag is commonly regarded as the undesired side effect of the lift generation in finite aspe...