Accession Number : AD0775892

Title :   Static Stability Wind-Tunnel Test of 18, 22, and 26 Caliber Cylinder- Ogive Bodies and an Aeroballistic Test Vehicle at Mach Numbers from 0.69 to 4. 24

Descriptive Note : Research rept.

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : Chaplin, Harvey

PDF Url : AD0775892

Report Date : 28 Jul 1953

Pagination or Media Count : 48

Abstract : The report presents the results of a wind tunnel investigation to determine the static stability of long bodies and an aeroballistic test vehicle at Mach numbers from 0.7 to 4.2.

Descriptors :   *CYLINDRICAL BODIES, *STATIC STABILITY, *SUBSONIC CHARACTERISTICS, *WIND TUNNEL TESTS, AEROBALLISTICS, AERODYNAMIC FORCES, CURVE FITTING, LENGTH, MOMENTS, PITCH(MOTION), ROCKETS, TEST VEHICLES

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE