Basic Concepts of Equations for the Aerodynamics of Bodies of Revolution PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Basic Concepts of Equations for the Aerodynamics of Bodies of Revolution PDF full book. Access full book title Basic Concepts of Equations for the Aerodynamics of Bodies of Revolution by Nikolai F. Krasnov. Download full books in PDF and EPUB format.
Author: Nikolai F. Krasnov
Publisher:
ISBN:
Category :
Languages : en
Pages : 169
Get Book Here
Book Description
Aerodynamic forces and moments; the basic features of very high velocity gas flow; the basic concepts and equations for determining the flow parameters; Basic relations for determining gas parameters behind a shock wave; Results from boundary-layer and heattransfer theory.
Author: Nikolai F. Krasnov
Publisher:
ISBN:
Category :
Languages : en
Pages : 169
Get Book Here
Book Description
Aerodynamic forces and moments; the basic features of very high velocity gas flow; the basic concepts and equations for determining the flow parameters; Basic relations for determining gas parameters behind a shock wave; Results from boundary-layer and heattransfer theory.
Author: Nikolaĭ Fedorovich Krasnov
Publisher: Elsevier Publishing Company
ISBN:
Category : Science
Languages : en
Pages : 930
Get Book Here
Book Description
A comprehensive technical treatise is provided on the aerodynamics of bodies of revolution from transonic to hypersonic speeds, covering all aspects of the subject, including transonic flow, linearized supersonic flow, Newtonian flow, rarefield gas and free-molecule flow, skin friction, heat transfer, and mass transfer. This English translation of a unique Russian textbook is provided with some corrections, references for all sources the editor could identify, redrawn figures, and an editor's introduction to each chapter summarizing and referencing pertinent material that has appeared since 1964, when the second edition was published. Krasnov's general approach assumes knowledge of the basic gas dynamic equations and applies them to solve aerodynamic problems. All important methods and techniques in modern aerodynamic theory are developed, with the aim of presenting practical methods for solving engineering problems. Results are usually given in the form of working equations, graphs, tables, or detailed sequential calculation methods. (Author).
Author: Robert C. Ried
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 968
Get Book Here
Book Description
Author: A. Mohammed
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: F. I. Frankl
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 14
Get Book Here
Book Description
The effect of acceleration of enlongated bodies of revolution upon the resistance in a compressible gas is investigated. It is assumed that the body produces only small disturbances in the flow so that the velocity potential satisfies the simple wave equation. The results of the analysis show that for accelerations not higher than 1000 meters per second2 and velocities comparable with the velocity of sound, the added pressures arising from the acceleration are negligibly small.
Author:
Publisher:
ISBN:
Category : Periodicals
Languages : en
Pages : 896
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1576
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 776
Get Book Here
Book Description
Author: Donn B. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Get Book Here
Book Description
