- Author
- Opalka, K. O.
- Title
- Wind-Tunnel Test of a Spinning, Low-Drag Projectile With Canted Bore Riders at Mach Numbers From 1.75 to 2.5.
- Coporate
- Army Ballistic Research Labs., Aberdeen Proving Ground, MD
- Report
- BRL-MR-2349, January 1974, 81 p.
- Distribution
- Available from National Technical Information Service
- Keywords
- wind tunnels | tunnel tests
- Identifiers
- canted bore riders; low-drag projectile; supersonic flow test; magnus moment and force