Projectile Base Bleed Technology; Part 2. User's Guide CMINT Computer Code, Version 5.04-BRL
Abstract
Detailed finite rate chemistry models for H2 and H2-CO combustion have been incorporated into a Navier-Stokes computer code and applied to flow field simulation in the base region of an M864 base burning projectile. Results without base injection were obtained using a low Reynolds number k-epsilon turbulence model and several mixing length turbulence models. The results with base injection utilized only the Baldwin-Lomax model for the Projectile forebody and the Chow wake mixing model downstream of the projectile base. A validation calculation was performed for a supersonic hydrogen-air burner using an H2 reaction set which is a subset of the H2-CO reaction set developed for the base combustion modeling. The comparison with the-available experimental data was good, and provides a level of validation for the technique and code developed Projectile base injection calculations were performed for a flat base M864 projectile at M infinity = 2. Hot air injection, H2 injection and H2-CO injection were modeled, and computed results show reasonable trends in the base pressure increase (base drag reduction), base corner expansion and downstream wake closure location.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1992
- Accession Number
- ADA258630
Entities
People
- Howard J. Gibeling
- Richard C. Buggeln