Computation of Supersonic Flow over Flying Configurations

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  • Author : Adriana Nastase
  • Publisher : Elsevier
  • Pages : 410 pages
  • ISBN : 9780080556994
  • Rating : 5/5 from 1 reviews
CLICK HERE TO GET THIS BOOK >>>Computation of Supersonic Flow over Flying Configurations

Download or Read online Computation of Supersonic Flow over Flying Configurations full in PDF, ePub and kindle. this book written by Adriana Nastase and published by Elsevier which was released on 07 July 2010 with total page 410 pages. We cannot guarantee that Computation of Supersonic Flow over Flying Configurations book is available in the library, click Get Book button and read full online book in your kindle, tablet, IPAD, PC or mobile whenever and wherever You Like. 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

Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations
  • Author : Adriana Nastase
  • Publisher : Elsevier
  • Release : 07 July 2010
GET THIS BOOK Computation of Supersonic Flow over Flying Configurations

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

Difference Methods for Initial Boundary Value Problems and Flow Around Bodies

Difference Methods for Initial Boundary Value Problems and Flow Around Bodies
  • Author : You-lan Zhu,Xi-chang Zhong,Bing-mu Chen,Zuo-min Zhang
  • Publisher : Springer Science & Business Media
  • Release : 29 June 2013
GET THIS BOOK Difference Methods for Initial Boundary Value Problems and Flow Around Bodies

Since the appearance of computers, numerical methods for discontinuous solutions of quasi-linear hyperbolic systems of partial differential equations have been among the most important research subjects in numerical analysis. The authors have developed a new difference method (named the singularity-separating method) for quasi-linear hyperbolic systems of partial differential equations. Its most important feature is that it possesses a high accuracy even for problems with singularities such as schocks, contact discontinuities, rarefaction waves and detonations. Besides the thorough description of the