Airbus Group India Private Limited

Airbus Engineering Centre India

Shreesh Mishra

Punit Tiwari

Sunil Kumar

Vikram Singh Mangat

Jose-Angel Hernanz Manrique

Madhusudana Reddy

Sandhya Jha

A system and method for extracting relevant computational data are disclosed. In one embodiment, one or more physical quantities and/or one or more functions of physical quantities of interest, associated with a larger volume, to be measured are identified. Further, any non-available identified functions of physical quantities are computed for each smaller volume of the larger volume using the available physical quantities in the computational data. Furthermore, regions in computational domain are identified along with ranges of identified physical quantities and functions of physical quantities of interest for carrying out the extraction from the computational data. Moreover, geometrical and connectivity information of smaller volumes associated with the identified regions/ranges that are obtained by filtering the computational data associated with the larger volume are obtained. Also, one or more clusters of smaller volumes are obtained using the obtained geometrical and connectivity information of smaller volumes associated with the identified regions/ranges.

System and method for extracting relevant computational data for design analysis and validation

A system and method for computing thermal boundary conditions from an unstructured computational fluid dynamics (CFD) simulation for a thermal simulation of a structural component are disclosed. The thermal boundary conditions include convective heat transfer coefficient (HTC) and reference temperature (T). In one embodiment, prism cells are formed to capture boundary layer substantially next to a wall of the structural component. Further, tetrahedral cells are formed to capture a diffused temperature layer substantially next to the formed last prism cell and in a direction normal to the wall. Furthermore, temperature of each of the prism cells is computed in the direction normal to the wall until a substantially first tetrahedral cell. In addition, the computed temperature of the prism cell that is substantially adjacent to the first tetrahedral cell is declared as the T. Also, the HTC is computed using the obtained T.

System and method for computing thermal boundary conditions from an unstructured CFD simulation on structural components

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Bengaluru, India

Shreesh Mishra