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Engineering
Aerothermodynamics
100%
Depth Ratio
100%
Cavity Flow
100%
Cavity Width
66%
Aerospace Vehicle
66%
Flow Model
33%
Primary Goal
33%
Thermal Protection
33%
Skin-Friction Coefficient
33%
Direct Simulation
33%
Hypersonic Flows
33%
Cavity Length
33%
Thermal Load
33%
Smooth Surface
33%
Aerodynamic Property
33%
Overprediction
33%
Continuum Approach
33%
Navier-Stokes Equation
33%
Ablation Rate
33%
Load Calculation
33%
Fabrication Tolerance
33%
Thermal protection systems
33%
INIS
comparative evaluations
100%
cavities
100%
length
50%
surfaces
50%
depth
50%
vehicles
50%
width
33%
protection
33%
augmentation
16%
space
16%
simulation
16%
tolerance
16%
increasing
16%
fabrication
16%
skin
16%
sensitivity
16%
sensors
16%
atmospherics
16%
altitude
16%
expansion
16%
monte carlo method
16%
imperfections
16%
installation
16%
ablation
16%
heat transfer
16%
plates
16%
earth atmosphere
16%
friction factor
16%
aerodynamics
16%
navier-stokes equations
16%
reentry
16%
hypersonic flow
16%
Keyphrases
Fabrication Tolerance
33%
Sensor Installation
33%