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title: 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
Preliminary Study of Integrated Aero-Propulsive Performance of Vehicle with CFD and Experiments
Comparison of Computation and Measurements in a Supersonic Cavity Combustor
Ionising Air in Thermo and Chemical Nonequilibrium Flow Behind a Plane Shock Wave
Mach 8 Ground Tests of the Hypermixer Scramjet for HyShot-IV Flight Experiment
Scramjet Driven MHD Power Demonstration Test - HVEPS Project Overview
Aero-Thermal Trade-Off Analysis of the Italian USV Re-Entry Flying Test Bed
Assesment of Synthetic Inflow Generation for Simulating Injection Into a Supersonic Crossflow
Effect of Nanoparticle Additives in Airbreathing Combustion
Fuel Composition Influence on Deposition from Endothermic Fuels
Plasma Torch Atomizer-Igniter for Supersonic Combustion of Liquid Hydrocarbon Fuels
Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0
Mission Trade-Off Analysis of the Italian USV Re-Entry Flying Test Bed
Measurement and Simulation of the Interface in a Low-Enthalpy Shock Tunnel
Simulations of Scramjet Starting and Establishment Time in an Expansion Tunnel
Flight Results from a Program to Develop a Freeflight Atmospheric Scramjet Test Technique
Design of Actively Cooled Panels for Scramjets
The Hy-V Scramjet Flight Experiment
Fast Mixing by Pulse Discharge in High-Speed Flow
Supersonic Streamwise Vortices Breakdown in Scramjet Combustor
Performances of a Rocket Chamber for the Combined-Cycle Engine at Various Conditions