Thermal Protection Sandwich Panel for Reentry Systems
A Safe, Economical and Versatile Space Flight Test Vehicle
Theoretical Investigation of the Compression Augmentation Effects of Variable Area Ejectors
Hypersonic/Supersonic Similitude of Energy Deposition for Wedge Profiles with Attached Shock Waves
Developing Optimized Trajectories Derived from Mission and Thermo-Structural Constraints
Simulation of Supercritical High Pressure Combustion for Advanced Propulsion Systems
Design and Analysis of a Single-stage Hypersonic Concept for Ultra-Rapid Global Travel
Influence of Gas Injection and Combustion on Start and Characteristics of Inlet
Experimental Investigations on the Self-Ignition of a Thermally Decomposed Endothermic Fuel
Transversal Electrical Discharge as a New Type of Flameholder
Computational Analysis of a 3D Hypersonic Intake for Experimental Testing at Mach 8
Rapid Conceptual Design and Analysis of Hypersonic Air-Breathing Missiles
Hybrid RANS/LES Study of Base-Bleed Flows in Supersonic Mainstream
Experimental Investigations of Scramjet Combustor Characteristics
Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight
DARPA/AF Falcon Program: The Hypersonic Technology Vehicle No.2 (HTV-2) Flight Demonstration Phase
A New Type of Low Drag Scramjet Combustor Based on Turbulent Mixing Enhancement