Journal of the Royal Aeronautical Society PDF Download
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1020
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1020
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Book Description
Author:
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 636
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Book Description
Includes entries for maps and atlases
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 856
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Book Description
Includes title page, table of contents, list of contributors, preface and all indexes of each book.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 666
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 986
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Book Description
Author:
Publisher:
ISBN:
Category : Aerospace planes
Languages : en
Pages : 526
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Book Description
Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
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Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author: Erian A. Baskharone
Publisher: McGraw Hill Professional
ISBN: 0071772359
Category : Technology & Engineering
Languages : en
Pages : 481
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Book Description
A practical, illustrated guide to thermal science A practical, illustrated guide to thermal science Written by a subject-matter expert with many years of academic and industrial experience, Thermal Science provides detailed yet concise coverage of thermodynamics, fluid mechanics, and heat transfer. The laws of thermodynamics are discussed with emphasis on their real-world applications. This comprehensive resource clearly presents the flow-governing equations of fluid mechanics, including those of mass, linear momentum, and energy conservation. Flow behavior through turbomachinery components is also addressed. The three modes of heat transfer--conduction, convection, and radiation--are described along with practical applications of each. Thermal Science covers: Properties of pure substances and ideal gases First and second laws of thermodynamics Energy conversion by cycles Power-absorbing cycles Gas power cycles Flow-governing equations External and internal flow structures Rotating machinery fluid mechanics Variable-geometry turbomachinery stages Prandtl-Meyer flow Internal flow, friction, and pressure drop Fanno flow process for a viscous flow field Rayleigh flow Heat conduction and convection Heat exchangers Transfer by radiation Instructor material available for download from companion website
Author: Yunus A. Çengel
Publisher:
ISBN: 9780071257640
Category : DVDs
Languages : en
Pages : 956
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Book Description
Covers the basic principles and equations of fluid mechanics in the context of several real-world engineering examples. This book helps students develop an intuitive understanding of fluid mechanics by emphasizing the physics, and by supplying figures, numerous photographs and visual aids to reinforce the physics.
Author: Luigi Crocco
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 236
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Book Description
The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.
