Knowledge of aerodynamic behavior of missile having cubical shape is important in connection with certain ordnance problems; study made to obtain experimental value for drag coefficient to cube in flight as function of Mach Number; air drag on two sizes of steel cubes, 1/4 and 3/8 in., determined.
Air drag on cubes at Mach numbers 0.5 to 3.5
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 2 ; p 83-84
1952
2 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Drag of Circular Cylinders at Transonic Mach Numbers
AIAA | 1977
|Pressure drag of bodies at Mach numbers up to 2.0
NTRS | 1953
|