Evaluation of Turboramjet Exhaust Systems from Scale Model Test Data
Boundary Conditions for Unsteady Supersonic Inlet Analyses
Tandem Transverse Hydrogen Gas Injection into a Supersonic Airflow
Active Control of Vortex Breakdown by a Spinning Wave Generator
Nozzle Effects on Linear Stability Behaviour of Combustors
Aerodynamic Inverse Design and Analysis for a Full Engine
Application of Functionally Gradient Materials to Scramjet Engines
Performance Improvement by Forward-Skewed Blading of Axial Fan Moving Blades
A Study on 3-D Velocity Distribution of Isothermal Flows Behind an Afterburner Flame Stabilizer
Study of a Pulse Ramjet Based on Twin Valveless Combustors Coupled to Operate in Antiphase
Two- and Three-Dimensional Prediffuser Combustor Studies with Air-Water Mixture
The Integration of the Rocket with the Ram-Scramjet as a Viable Transatmospheric Accelerator
LIF Visualization of 3-Dimensional Hypersonic Mixing
Influence of Chemical Kinetics Effects in Nozzles Shape Design
A Study of the Stability of Vortical Structures in Supersonic Inlets