Scramjet Experiments in an Expansion Tunnel: Evaluated Using a Quasi-Steady Analysis Technique
Performance Analysis of a Mach 12 REST Scramjet at Off-Design Conditions
Numerical and Experimental Investigation of a Two-Staged Supersonic Combustion Chamber
Influence of Sidewall Compression on Hypersonic Intake Performance
Effects of Localized Flow Heating by DC-Arc Discharge Ahead of Non-Slender Bodies
Experimental and Numerical Studies of a Strut Injector for Round Scramjet Combustors
Rate-Based Sensing Concepts for Heat Flux and Property Estimation, and Transition Detection
Local Enthalpy Estimation in Plasma flows Using an Improved Mass Injection Probe
Flight Dynamics of a Hypersonic Vehicle During Inlet Unstart
In-Flight Mapping of Heating on a Hypersonic Nose Cone
3-D Influences on Nominally 2-D Strut Injection Supersonic Combustion
LAPCAT 2 - Axisymmetric Concept for a Mach 8 Cruiser Preliminary Design and Performance Assessment
TBCC Hypersonic Performance: Effect of Inlet Entropy
Computation and Analysis of Aeroheating on Hypersonic Inlet Leading Edge
Control of Supersonic Flow in Compression Ramp by Near-Surface Electrical Discharge
Drag Reduction by Energy Deposition in Hypersonic Flows
Preliminary Design and Simulation of Reflected Shock Tunnel in Taiwan