Ignition Characteristics of a New High-Energy Density Fuel in High-Speed Flows
Effects of the Chemical Reaction Model on Calculations of Supersonic Combustion Flows
Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications
A Unique, Mach 6 Enthalpy, Non-Vitiated Facility for Hypersonic Aerodynamics Research
Experiments in Thermosensitive Cavitation of a Cryogenic Rocket Propellant Surrogate
Sub-to-Supercritical Mixing in Single and Dual Component Systems
SUB-TO-SUPERCRITICAL MIXING AND CORE LENGTH ANALYSIS OF A SINGLE ROUND JET
SUB-TO-SUPERCRITICAL JET MIXING AND CORE LENGTH ANALYSIS
Experimental Study of Subcritical to Supercritical Jet Mixing
Mixing and Mass Exchange for Cavities in Supersonic Flows (AIAA 2014-2951)