Dynamic Stability Investigation of Two Right Circular Cylinders in Axial Free Flight at Mach Numbers from 0.4 to 1.7 Fineness-Ratio- 2.56 Cylinder and Fineness-Ratio-4.0 Cylinder with Flared Afterbody
1957
48 pages
Report
No indication
English
Aerodynamics , Circular cylinder , Dynamic stability , Free flight , Longitudinal stability , Afterbody , Axial , Body , Booster , Circular , Cylinder , Dynamic , Fineness , Flare , Free , Longitudinal , Mach number , Model , Ratio , Reynolds number , Right , Rocket , Stability