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Direct numerical simulation of BOLT hypersonic flight vehicle
John Thome
,
Anubhav Dwivedi
,
Joesph W. Nichols
,
Graham V. Candler
Aerospace Engineering and Mechanics
Electrical and Computer Engineering
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
41
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Scopus citations
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Keyphrases
Boundary Layer Transition
100%
Complex Flow
25%
Complex Geometric Features
25%
Complex Geometry
25%
Crossflow Instability
25%
Direct numerical Simulation
100%
Distributed Surface Roughness
25%
Flight Experiment
25%
Flow Features
25%
Flow Field
25%
Flow Physics
25%
Flow Structure
25%
Heat Flux
25%
High Heat Flux
25%
High Reynolds number
25%
High-speed Vehicle
25%
Hypersonic Flight Vehicle
100%
Instability Mechanism
25%
Invalid
25%
Laminar Boundary Layer
50%
Low Reynolds number
25%
Mach number
25%
Mack Mode
25%
Pressure Disturbance
25%
Reynolds number
25%
Simplifying Assumption
25%
Skin Friction Drag
25%
Small Amplitude
25%
Stability Analysis
50%
Transition Flight
25%
Turbulent Boundary Layers
25%
Turbulent State
25%
Unsteady Pressure
25%
Vehicle Configuration
25%
Engineering
Boundary Layer Transition
100%
Direct Numerical Simulation
100%
Flow Distribution
25%
Flow Physic
25%
Flow Structure
25%
Geometric Feature
25%
Heat Flux
50%
High Reynolds Number
25%
Hypersonic Flight Vehicle
100%
Instability Mechanism
25%
Laminar Boundary Layer
50%
Mach Number
25%
Realization
25%
Simplifying Assumption
25%
Skin Friction Drag
25%
Stability Analysis
50%
Turbulent Boundary Layer
25%