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
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 28, 1953
- Accession Number
- AD0775892
Entities
People
- Harvey Chaplin
Organizations
- Naval Ordnance Laboratory