Plasma Driven Hypersonic Testing
Abstract
The objective of the proposed effort is to develop a novel, compact experimental platform and associated diagnostics to quantitatively investigate a variety of hypersonic phenomena (at Mach numbers approaching 10) in a laboratory environment using high velocity plasma flows generated by a z-pinch pulsed discharge plasma generator.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Feb 06, 2017
- Source ID
- FA95501710036
Entities
People
- Simon Bland
Organizations
- Air Force Office of Scientific Research
- Imperial College London
- United States Air Force