PERFORMANCE ANALYSIS OF THE APL HYPERSONIC GUN TUNNEL,
Abstract
Performance calculations foor the APL Hypersonic Gun Tunnel are presented. These calculations are limited to initial pump tube pressures of 1 atmosphere and temperatures of 290 K. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1964
- Accession Number
- AD0458368
Entities
People
- R. A. Makofski
Organizations
- Johns Hopkins University