Add to ORKGSeveral variational problems involving optimum wing and body combinations having minimum wave drag for different kinds of geometrical restraints are analyzed. Particular attention is paid to the effect on the wave drag of shortening the fuselage and, for slender axially symmetric bodies, the effect of fixing the fuselage diameter at several points or even of fixing whole portions of its shape
This paper focuses on the drag characteristics of optimally span-loaded planar, winglet-ted, and C-w...
Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking...
Abstract. The optimization strategy is an own, two times enlarged variational method, which is able ...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
The word “interference ” is usually associated with adverse effects. However, interference between t...
abstract: This paper describes an aircraft design optimization tool for wave drag reduction. The too...
The aerodynamical optimal design (OD) of the shape of flying configurations (FCs) can be improved by...
This paper presents the wave-drag characteristics of an over-the-wing nacelle con guration. The ow...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
This paper focuses on the drag characteristics of optimally span-loaded planar, winglet-ted, and C-w...
Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking...
Abstract. The optimization strategy is an own, two times enlarged variational method, which is able ...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
The word “interference ” is usually associated with adverse effects. However, interference between t...
abstract: This paper describes an aircraft design optimization tool for wave drag reduction. The too...
The aerodynamical optimal design (OD) of the shape of flying configurations (FCs) can be improved by...
This paper presents the wave-drag characteristics of an over-the-wing nacelle con guration. The ow...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
This paper focuses on the drag characteristics of optimally span-loaded planar, winglet-ted, and C-w...
Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking...
Abstract. The optimization strategy is an own, two times enlarged variational method, which is able ...