An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separation from slender rods mounted to extend forward along the axes of symmetry of blunt-nosed bodies. The mechanism of the separation and its governing criteria are discussed. Drag data at a Mach number of 2.72 for various rod lengths and nose radii at an angle of attack of zero degrees are presented. It was found that the drag coefficients of blunt noses could be appreciably reduced by the use of protruding rods. Criteria for rod length which gives lowest drag are given. (author)
Results are presented of the drag tests of six bodies of revolution with systematically varying shap...
An experimental investigation concerned primarily with the extension of test data on the drag of rev...
Values of total-drag coefficient were measured for two fin-stabilized, blunt-nose bodies of revoluti...
An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separ...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
A new nose shape that was determined using the penetration mechanics to have the least penetration d...
Values of total drag coefficient were measured for four round-nosed bodies of revolution in free fli...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
The subject of this paper is the drag of the nose section of bodies of revolution at zero angle of a...
The three papers collected here are: 'The Effect of Nose Shape on the Drag of Bodies of Revolution a...
Use of flow separation on a rod projecting upstream of a blunt body to decelerate the supersonic str...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation has been made with rocket-propelled models in free flight to determine the external...
An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...
Results are presented of the drag tests of six bodies of revolution with systematically varying shap...
An experimental investigation concerned primarily with the extension of test data on the drag of rev...
Values of total-drag coefficient were measured for two fin-stabilized, blunt-nose bodies of revoluti...
An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separ...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
A new nose shape that was determined using the penetration mechanics to have the least penetration d...
Values of total drag coefficient were measured for four round-nosed bodies of revolution in free fli...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
The subject of this paper is the drag of the nose section of bodies of revolution at zero angle of a...
The three papers collected here are: 'The Effect of Nose Shape on the Drag of Bodies of Revolution a...
Use of flow separation on a rod projecting upstream of a blunt body to decelerate the supersonic str...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation has been made with rocket-propelled models in free flight to determine the external...
An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...
Results are presented of the drag tests of six bodies of revolution with systematically varying shap...
An experimental investigation concerned primarily with the extension of test data on the drag of rev...
Values of total-drag coefficient were measured for two fin-stabilized, blunt-nose bodies of revoluti...