Add to ORKGThe observed flow field about slender inclined bodies of revolution is compared with the calculated characteristics based upon potential theory. The comparison is instructive in indicating the manner in which the effects of viscosity are manifest. Based on this and other studies, a method is developed to allow for viscous effects on the force and moment characteristics of bodies. The calculated force and moment characteristics of two bodies of high fineness ratio are shown to be in good agreement, for most engineering purposes, with experiment. (author)
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
Equations are derived for the orientation of a spheroid in Couette flow when an electric field is ap...
Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating...
The observed flow field about slender inclined bodies of revolution is compared with the calculated ...
The simplified solution for the pressure distribution of slender inclined bodies of revolution is de...
Experimental force, moment, and center-of-pressure variations for a large number of bodies of revolu...
In this paper we shall attempt to review the existing information, both theoretical and experimenta...
Pressure distributions and force characteristics have been determined for a body of revolution consi...
This research addresses the difficulties in determining the manoeuvring characteristics of a slender...
An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...
The method of characteristics has been applied for the determination of the supersonic-flow properti...
Twelve different slender bodies were tested at Mach 2 and 3 in the angle of attack range of 20 and 5...
Effects of Reynolds number and angle of attack on the pressure distribution and normal-force charact...
Visual-flow studies were made of the behavior of the vortices which form in the separated flow regio...
"It is shown that adequate means are available for calculating inviscid direct and induced pressures...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
Equations are derived for the orientation of a spheroid in Couette flow when an electric field is ap...
Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating...
The observed flow field about slender inclined bodies of revolution is compared with the calculated ...
The simplified solution for the pressure distribution of slender inclined bodies of revolution is de...
Experimental force, moment, and center-of-pressure variations for a large number of bodies of revolu...
In this paper we shall attempt to review the existing information, both theoretical and experimenta...
Pressure distributions and force characteristics have been determined for a body of revolution consi...
This research addresses the difficulties in determining the manoeuvring characteristics of a slender...
An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...
The method of characteristics has been applied for the determination of the supersonic-flow properti...
Twelve different slender bodies were tested at Mach 2 and 3 in the angle of attack range of 20 and 5...
Effects of Reynolds number and angle of attack on the pressure distribution and normal-force charact...
Visual-flow studies were made of the behavior of the vortices which form in the separated flow regio...
"It is shown that adequate means are available for calculating inviscid direct and induced pressures...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
Equations are derived for the orientation of a spheroid in Couette flow when an electric field is ap...
Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating...