Computational methods to optimize Supersonic Nozzles: Algorithms and Program Complex - Couverture souple

Gaissinski, Igor; Stricker, Josef

 
9783659396045: Computational methods to optimize Supersonic Nozzles: Algorithms and Program Complex
Couverture souple
ISBN 10 : 3659396044 ISBN 13 : 9783659396045
Editeur : LAP LAMBERT Academic Publishing, 2013

Synopsis

The book is devoted to calculation methods of a converging-diverging nozzle used in propulsion and the high velocity flow. The algorithms and programs given in the book are intended to help engineers and students to design and calculate the nozzle parameters to provide optimal parameters for compressible supersonic flows. The present monograph is a tutorial (handbook) to calculate and determine the optimal parameters for converging-diverging nozzles provided supersonic flow. The main program consists from three main parts: programs for calculation the profile of the Contraction zone, EOD code for the flow in the Contraction zone, the program Rott-Crabtree for calculation the pressure gradient Pohlhausen parameter, the program for the aerodynamic design of axisymmetric and two-dimensional nozzles for supersonic and hypersonic wind tunnels, programs for solving laminar, transitional, or turbulent compressible boundary layer equations for two-dimensional and axisymmetric flow, and the program to obtain hypersonic boundary layer stability. The book is designed to be an instrument for students and scientists interested in study supersonic flow and high-temperature gas dynamics.

Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.

Présentation de l'éditeur

The book is devoted to calculation methods of a converging-diverging nozzle used in propulsion and the high velocity flow. The algorithms and programs given in the book are intended to help engineers and students to design and calculate the nozzle parameters to provide optimal parameters for compressible supersonic flows. The present monograph is a tutorial (handbook) to calculate and determine the optimal parameters for converging-diverging nozzles provided supersonic flow. The main program consists from three main parts: programs for calculation the profile of the Contraction zone, EOD code for the flow in the Contraction zone, the program Rott-Crabtree for calculation the pressure gradient Pohlhausen parameter, the program for the aerodynamic design of axisymmetric and two-dimensional nozzles for supersonic and hypersonic wind tunnels, programs for solving laminar, transitional, or turbulent compressible boundary layer equations for two-dimensional and axisymmetric flow, and the program to obtain hypersonic boundary layer stability. The book is designed to be an instrument for students and scientists interested in study supersonic flow and high-temperature gas dynamics.

Biographie de l'auteur

Igor Gaissinski, Ph.D, Senior Scientist, TECHNION, Faculty of Aerospace Engineering, D.Sc, 1989, Physics & Mathematics., Russian Academy of Sciences (USSR). Josef Stricker, Ph.D, Associate Professor, TECHNIONFaculty of Aerospace Engineering, Ph.D, 1969, Physics, Hebrew University (Jerusalem).

Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.

Éditeur
LAP LAMBERT Academic Publishing
Date d'édition
2013
Langue
anglais
ISBN 10 
3659396044
ISBN 13 
9783659396045
Reliure
Broché
Nombre de pages
400
Coordonnées du fabricant
non disponible
Personne responsable
KreGa Onlinehandel GmbH
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