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Transverse jet injection into a supersonic turbulent cross-flow
Z.A. Rana, B. Thornber, D. Drikakis
Faculty Of Engineering
Research output
:
Contribution to journal
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Article
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peer-review
145
Citations (Scopus)
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Dive into the research topics of 'Transverse jet injection into a supersonic turbulent cross-flow'. Together they form a unique fingerprint.
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Physics
Cross Flow
100%
Injection
100%
Large Eddy Simulation
100%
Supersonics
100%
Turbulent Boundary Layer
66%
Stability
66%
Shear Layer
66%
Combustion Chamber
66%
Work
33%
Mathematical Method
33%
Penetration
33%
Utilities
33%
Extrapolation
33%
Physics
33%
Utilization
33%
Mixing
33%
Free Flow
33%
Supersonic Combustion Ramjet Engines
33%
Aerospace Engineering
33%
Eddy
33%
Pressure Distribution
33%
Fuel Injection
33%
Noise Control
33%
Volume
33%
Engineering
Large Eddy Simulation
100%
Demonstrates
66%
Fluid Dynamics
66%
Accuracy
66%
Fluid
66%
Fields
33%
Combustion Chamber
33%
Mixing
33%
Centered Scheme
33%
Vortex
33%
Cavity
33%
Computational Resource
33%
Initial Condition
33%
Stability
33%
Reynolds Stress
33%
Simulation Technique
33%
Freestream
33%
Vectors
33%
Applications
33%
Turbulent Kinetic Energy
33%
Fuel Injection
33%
Efficiency
33%
Pressure Distribution
33%
Aerospace Engineering
33%
Numerical Method
33%
Control Systems
33%
Conservation Law
33%
Stages
33%
Earth and Planetary Sciences
Digital Filter
33%
Supersonic Combustion Ramjet Engine
33%
Fuel Injection
33%
Rocket Thrust
33%
Noise Control
33%
Thrust Vector Control
33%
Shear Layer
33%
Turbulent Boundary Layer
33%