ANALYTICAL STUDY OF NON-EQUILIBRIUM FLOW IN HYPERSONIC NOZZLES USING A SIMPLIFIED MODEL FOR AIR,
Abstract
An analytical method is developed for calculating the one-dimensional flow in hypersonic nozzles of a simplified model of air, which takes into account dissociational and vibrational non-equilibrium effects using the sudden-freezing hypothesis of Bray. The model gas consists of a mixture of oxygen, treated as an ideal dissociating gas, in an inert nitrogen diluent. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 04, 1967
- Accession Number
- AD0649188
Entities
People
- K. R. Enkenhus
Organizations
- Naval Ordnance Laboratory