Solution of Non-isoenergetic Supersonic Flows by Method of Characteristics, Volume 3 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 Solution of Non-isoenergetic Supersonic Flows by Method of Characteristics, Volume 3 PDF full book. Access full book title Solution of Non-isoenergetic Supersonic Flows by Method of Characteristics, Volume 3 by . Download full books in PDF and EPUB format.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 170
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 170
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 208
Get Book Here
Book Description
Author: T. Hsieh
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 64
Get Book Here
Book Description
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder at zero incidence in the transonic and low supersonic Mach number range (M = 0.7 to 2.0). For M less than or equal to 1, the method used is a combination of the time-dependent solution for the hemispherical nose portion and the method-of-characteristics solution for the cylindrical body portion. The relaxation method has been used for Mach numbers from 0.7 to 1.3. Experimental results indicate a strong interaction of the shock and boundary layer for M approximately equal to 0.8.
Author:
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 470
Get Book Here
Book Description
Author: Oleksandr Girin
Publisher: Springer Nature
ISBN: 3031112628
Category : Science
Languages : en
Pages : 316
Get Book Here
Book Description
Compressibility is a property inherent in any material, but it does not always manifest itself. Experience suggests that it affects the medium motion only at velocities comparable to the speed of sound. Why do we study compressibility? It turns out that in order to calculate the aircraft streamlining or the internal flow in its engine, or the shell muzzle velocity, or the dynamic load of a shock wave from an accidental blast on a structural element, and in many other cases it is necessary to know and understand the laws of the Dynamics of Compressible Media (DCM) and be able to apply them in practice. This textbook is designed to help readers achieve this goal and learn the basics of DCM. This field of knowledge is high-tech and always focuses on the future: modern developments of hypersonic aircraft, designing more advanced structural elements for airplanes and helicopters, calculating the car aerodynamics, etc. Paradoxes have always given impetus to the search for new technological devices. Unusual effects in DCM include the flow chocking in supersonic outflow from reservoirs (Sect.2.2); the shock wave formation inside an initially smooth flow (Sect.5.3); the generation of a "spallation saucer" of armor inside a tank when a shell hits it (Sect.5.5); the dog-leg of a plane discontinuity surface at shockwave reflection from a rigid wall (Sec.8.1). The way to understand these and other effects is through the creation of quantitative models of a moving compressible fluid.
Author: United States. National Technical Information Service
Publisher:
ISBN:
Category : Computer programs
Languages : en
Pages : 336
Get Book Here
Book Description
Author: D. Küchemann
Publisher: Elsevier
ISBN: 1483148874
Category : Technology & Engineering
Languages : en
Pages : 481
Get Book Here
Book Description
Progress in Aeronautical Sciences
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 708
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 324
Get Book Here
Book Description
