Pulse Detonation Physiochemical and Exhaust Relaxation Processes
Abstract
The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significant impact upon performance, will be explored in order to achieve basic understanding of the relationships between detonations, nozzles, and multiple detonation tube interactions.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 19, 2001
- Accession Number
- ADP012098
Entities
People
- Fred Schauer
Organizations
- Air Force Research Laboratory