The split-skirt is a variable drag bomb stabilizer which is being studied by the U. S. Naval Ordnance Laboratory. This report gives the results of static and dynamic wind-tunnel tests of several configurations formed from various combinations of three noses and four skirts. (Author)
The Aerodynamic Characteristics of an Ogive Cylinder with Split-Skirt Stabilizer at Subsonic, Transonic and Supersonic Speeds
1965
79 pages
Report
No indication
English
Fluid Mechanics , Bombs , Bomb fins , Stabilization systems , Aerodynamic characteristics , Stability , Nose cones , Ogives , Aerodynamic configurations , Drag , Force(Mechanics) , Moments , Aerodynamic loading , Pitch(Motion) , Damping , Angle of attack , Roll , Yaw , Wind tunnel models , Model tests , Performance(Engineering) , Experimental data , Subsonic characteristics , Transonic characteristics , Supersonic characteristics
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