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Fan simuilation
NASA rotor, 37 passages
Low Re, thermally driven flow
Fuel sub assembly
High lift devices flow
MAV
Meshes for wing n flap
Single Passage
Temperture in sub assembly
Wing body
Dish Antenna
Pressure Contours
Streamlines showing wake
Mass conservation affects range of velocities in pressure based solvers.
Hypersonic Validation
Geometry and a section showing velocity-magnitude contours.
Adaptive mesh refinement in oct-tree grid.
Conjugate heat transfer studies with 25 million pure hex cells using CFDExpert(TM)
Geometry - CFD Analysis for Fan Duct Design and/or Optimization
A partially opened multi-linked file, seen in ViewZ.
Mach plot for double ramp Hypersonic air intake.
Production Drawings.
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