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Hypersonic nozzle analysis using an excluded volume equation of state
Graham V. Candler
Aerospace Engineering and Mechanics
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
66
Scopus citations
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Dive into the research topics of 'Hypersonic nozzle analysis using an excluded volume equation of state'. Together they form a unique fingerprint.
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Keyphrases
Boundary Layer
33%
Cell Aspect Ratio
33%
Chemical Reaction
33%
Compressibility Correction
33%
Computational Methods
33%
Data Parallelism
33%
Energy Chemical
33%
Equation of State
100%
Excluded Volume
100%
Finite Rate
33%
Flux Vector Splitting
33%
Grid Stretching
33%
High-pressure Effects
33%
High-pressure Nozzle
33%
Hypersonic Nozzle
100%
Implicit Information
33%
Low Power Dissipation
33%
Machine Zero
33%
Non-ideality
33%
Nozzle
66%
Nozzle Flow
33%
Numerics
33%
Parallel Lines
33%
Rate-based Model
33%
Relaxation Method
33%
Spalart-Allmaras Turbulence Model
33%
Steger-warming
33%
Stretched Grid
33%
Turbulent Boundary Layers
33%
Vibrational Energy Relaxation
33%
Volume Equation
100%
Mathematics
Aspect-Ratio
50%
Boundary Layer
100%
Dimensional Time
50%
Experimental Data
50%
Flux Vector
50%
Numerics
50%
Parallel Line
50%
Relaxation Method
50%
Time Step
50%
Physics
Aspect Ratio
33%
Boundary Layer
33%
Compressibility
33%
Computational Method
33%
Equations of State
100%
Flux Vector Splitting
33%
Hypersonics
100%
Nozzle Flow
33%
Turbulence Model
33%
Turbulent Boundary Layer
33%
Earth and Planetary Sciences
Boundary Layer
33%
Compressibility
33%
Computational Method
33%
Equations of State
100%
Hypersonic Nozzle
100%
Nozzle Flow
33%
Nozzle Walls
33%
Turbulence Model
33%
Turbulent Boundary Layer
33%
Engineering
High pressure effects
33%