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
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
A concept for interrelating the wave drags of wing-body combinations at supersonic speeds with axial...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
The minimization of inviscid fluid drag is studied for aerodynamic shapes satisfying the conditions ...
A procedure for tailoring a blended wing-body configuration to reduce its computed wave drag is desc...
The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either i...
The word “interference ” is usually associated with adverse effects. However, interference between t...
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
Comparisons are made of experimental and theoretical zero-lift wave drag for several nose shapes, wi...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
For a given wing and supersonic Mach number, the problem of shaping an adjoining fuselage so that th...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
A concept for interrelating the wave drags of wing-body combinations at supersonic speeds with axial...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
The minimization of inviscid fluid drag is studied for aerodynamic shapes satisfying the conditions ...
A procedure for tailoring a blended wing-body configuration to reduce its computed wave drag is desc...
The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either i...
The word “interference ” is usually associated with adverse effects. However, interference between t...
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
Comparisons are made of experimental and theoretical zero-lift wave drag for several nose shapes, wi...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...