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Atmospheric reentry modelling using an open source DSMC code
Rodrigo Cassineli Palharini
Mechanical And Aerospace Engineering
Research output
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Thesis
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Doctoral Thesis
1501
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Engineering
Aerodynamic Surface
25%
Aerothermodynamics
25%
Bottom Surface
25%
Cavity
100%
Cavity Length
25%
Codes
100%
Depth Ratio
25%
Development
25%
Direct Simulation
100%
Flow Regime
25%
Flow Separate
25%
Heating
25%
Joints (Structural Components)
25%
Kinetic
50%
Models
50%
Nonequilibrium
25%
Numerical Method
25%
Numerical Technique
25%
Prediction
25%
Quantity
25%
Rarefied Gas
25%
Re-Entry Vehicle
25%
Structure Surface
25%
Surfaces
25%
System Protection
75%
Thermal Protection
75%
Physics
Hypersonic Reentry
25%
Micrometeorites
25%