Majumder, Sutrisha
(2015)
Development of a General-Purpose Compressible Flow AnuPravaha Based Solver using an Implicit Method (Thermo Fluids).
Masters thesis, Indian Institute of Technology Hyderabad.
Abstract
The design of aerospace vehicles requires a detailed knowledge of the interactions between flight surfaces and the ambient atmosphere through which they pass. The resulting aerodynamic pressure as well as heating loads are among the critical parameters inherent to a successful design. Insight into these conditions is obtained through a mix of analytical, computational and ground based experimental techniques. The recent paradigm shift embraced by the motto faster, better, cheaper calls for continual improvement in these areas through a greater understanding of the physical processes involved.
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