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Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that 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 aerodynamic characteristics of flying configurations
- Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
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