Accession Number:

AD0253540

Title:

DRAG AND STABILITY DATA OBTAINED FROM FREE-FLIGHT RANGE FIRINGS WITHIN THE MACH NUMBER RANGE OF 0.4 TO 3.0 FOR SEVERAL CYLINDRICAL CONFIGURATIONS

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1960-10-03

Pagination or Media Count:

6.0

Abstract:

Tests were conducted at the Naval Ordnance Laboratory on several cylindrical configurations to determine their drag and stability characteristics. The configurations consisted of four types three types of fin-cylinders and an offset C.G. cylinder, i.e., one whose C.G. is off the axis of the cylinder. These were fired within the Mach number range of 0.4 to 3.0. Drag and stability coefficients were obtained for the configurations. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE