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| | Aero Dynamics |
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| | | Computational Fluid Dynamics | | CFD Tools at ADA | - Multi-block Euler Codes for steady/unsteady flow over complete configurations(AMES/HYENA/IMAGE)
- Multi-block/Unstructured Euler/Navier-Stokes code for Aircraft/Intake Duct
- Cartesian grid Euler code for complete Aircraft (PARAS)
- Finite volume electromagnetics code(CFD-CEM)
- Full potential field integral code with Cartesian grid for store separation studies (FIM/AMAR)
- Steady/Unsteady Panel code for complete aircraft
- Surface modeling and Grid generation modules
- Grid adaptation
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Visualization of structured/unstructured grids and flow field
| CFD Applications for LCA | - Wing design & fuselage shape optimization
- Evaluation of incremental changes in configuration
- Wave drag prediction
- Optimisation of Leading Edge Slat schedule
- Aerodynamic load distribution on major components
- Flow field (angularity & pressure) at the Air Data Sensor locations
- Store separation studies
- Viscous flow analysis in Intake Duct
- Aerodynamic devices like fore-plane, LEVCON etc.
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RCS prediction of Aircraft configuration
| High Performance Parallel Computers at ADA for CFD | - 16 Node, ANUP-16, P-III,550 MHz (5 G Flops)
- 32 Node, NAS, P-III, 800 MHz (15 G Flops)
- 64 Node, HPC-64, P-III, 1GHz (35 G Flops)
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