Add to ORKGA concept for interrelating the wave drags of wing-body combinations at supersonic speeds with axial developments of cross-sectional area is presented. A swept-wing-indented-body combination designed on the basis of this concept to have significantly improved maximum lift-drag ratios over a range of transonic and moderate supersonic speeds is described. Experimental results have been obtained for this configuration at Mach numbers from 0.80 to 2.01. Maximum lift-drag ratios of approximately 14 and 9 were measured at Mach numbers of 1.15 and 1.41, respectively
Numerical procedure for analyzing and designing wings and wing-body combinations in supersonic flo
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
Wind-tunnel force tests of a number of wing-body combinations designed for high lift-drag ratio at a...
The effects of changing indentation design Mach number on the aerodynamic characteristics of a 45 de...
This paper is concerned primarily with the application of the "area rule" to the interpretation and ...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
An investigation was made of the effects of body shape on the drag of a 45 deg sweptback-wing-body c...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calcula...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
The importance of the lift to drag ratio is well known to all aircraft designers since it gives, to ...
Numerical procedure for analyzing and designing wings and wing-body combinations in supersonic flo
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
Wind-tunnel force tests of a number of wing-body combinations designed for high lift-drag ratio at a...
The effects of changing indentation design Mach number on the aerodynamic characteristics of a 45 de...
This paper is concerned primarily with the application of the "area rule" to the interpretation and ...
Several variational problems involving optimum wing and body combinations having minimum wave drag f...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
An investigation was made of the effects of body shape on the drag of a 45 deg sweptback-wing-body c...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calcula...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
The importance of the lift to drag ratio is well known to all aircraft designers since it gives, to ...
Numerical procedure for analyzing and designing wings and wing-body combinations in supersonic flo
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
An analysis, based on the linearized thin-airfoil theory for supersonic speeds, of the wave drag at ...