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Название: Computation of Supersonic Flow over Flying Configurations
Автор: Nastase A.
Аннотация:
This high level aerospace reference book will be useful for undergraduate, and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows.
* Computational work and experimental results show the real world application of computational results
* Easy computation and visualization of inviscid and viscous aerodynamis characteristics of flying configerations
* Includes a fully optimized and integrated design for a proposed supersonic transport aircraft