Add to ORKGLet L, R, Y be arbitrary real constants. A wing with fixed span which produces lift L, roll moment R, yaw moment Y and which has minimal induced drag D is wanted. This problem arises in airplane engineering. It is solved by means of Prandtl's lifting line theory combined with computation.
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
The problem of a wing placed in a flow that is nonuniform in the spanwise direction is of interest t...
AbstractIn a famous report about the induced drag of multiplanes, L. Prandtl conceived the Best Wing...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
This paper focuses on the drag characteristics of optimally span-loaded planar, winglet-ted, and C-w...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
In order to fly, an aircraft of a given weight needs to produce an equal but opposite force to this w...
The aim of this paper is to evaluate the theoretical limit of the induced drag in non-planar wing co...
The classic minimum induced drag spanload is not necessarily the best choice for an aircraft. For a ...
For a wing in steady level flight, the lift distribution that minimizes induced drag depends on a tr...
Because the wing-structure weight required to support the critical wing section bending moments is a...
Summary The induced drag of non-planar wings is compared to that of planar wings which result fro...
In this article history and development of calculation methods of wing characteristics are presented...
The solution of the lifting line equation Prandtl in wing theory is viewed afresh. Some new aspects ...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
The problem of a wing placed in a flow that is nonuniform in the spanwise direction is of interest t...
AbstractIn a famous report about the induced drag of multiplanes, L. Prandtl conceived the Best Wing...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
This paper focuses on the drag characteristics of optimally span-loaded planar, winglet-ted, and C-w...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
In order to fly, an aircraft of a given weight needs to produce an equal but opposite force to this w...
The aim of this paper is to evaluate the theoretical limit of the induced drag in non-planar wing co...
The classic minimum induced drag spanload is not necessarily the best choice for an aircraft. For a ...
For a wing in steady level flight, the lift distribution that minimizes induced drag depends on a tr...
Because the wing-structure weight required to support the critical wing section bending moments is a...
Summary The induced drag of non-planar wings is compared to that of planar wings which result fro...
In this article history and development of calculation methods of wing characteristics are presented...
The solution of the lifting line equation Prandtl in wing theory is viewed afresh. Some new aspects ...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
The problem of a wing placed in a flow that is nonuniform in the spanwise direction is of interest t...
AbstractIn a famous report about the induced drag of multiplanes, L. Prandtl conceived the Best Wing...