SFFSTAB: A Computer Program to Calculate the Aerodynamic Stability of a Self-Forging Fragment.
Abstract
An aerodynamic stability computer program (SFFSTAB) has been developed for calculating the spin rate required for stabilization of a self-forging fragment. An aerodynamic stability criterion which combined gyroscopic and dynamic stability was used together with a technique for calculating aerodynamic coefficients. SFFSTAB is a useful tool for conducting aerodynamic stability parameter studies for different fragment shapes. Complete documentation of the computer program including sample problem, flowchart and FORTRAN listing is provided. Keywords: explosions, fragments, computer program.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1987
- Accession Number
- ADA179857
Entities
People
- C. A. Weickert
Organizations
- Defence Research and Development Canada