کتاب های پیشرانش

وضعیت
موضوع بسته شده است.

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
سلام،



این کتاب شامل مراحل طراحی یک جت مسافربری از ابتدا تا انتهاست.از طراحی مفهومی آم شروع کرده و به آنالیز هزینه ها ختم می شود.

http://rapidshare.com/files/79583835/Civil_Jet_Aircraft_Design.rar

Password:ebookee[at]gmail.com
 
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
کتاب های پیشرانش

سلام،
تاپیک کتاب های پیشرانش:
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Fundamentals of Jet Propulsion with Applications

Fundamentals of Jet Propulsion with Applications



Fundamentals of Jet Propulsion with Applications (Cambridge Aerospace Series)
By Ronald D. Flack
* Publisher: Cambridge University Press
* Number Of Pages: 658
* Publication Date: 2005-04-25
* ISBN-10 / ASIN: 0521819830
* ISBN-13 / EAN: 9780521819831
Book Description:
Fundamentals of Jet Propulsion with Applications is an introductory text in air-breathing jet propulsion including ramjets, turbojets, turbofans, and propjets. Aimed at upper-level undergraduate and graduate students, the book provides coverage of the basic operating principles, from cycle analysis through component design and system matching. A basic understanding of fluid mechanics and thermodynamics is assumed, although many principles are thoroughly reviewed. Numerous examples and nearly 300 homework problems based on modern engines make this book an ideal teaching tool, as well as a valuable reference for practicing engineers. A CD included with the book contains example files and software to support the text​

39.74 MB

http://mihd.net/0ta2i9


depositfiles.com



easy-share




filefactory


 
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
(Elements of Propulsion: Gas Turbines And Rockets (Aiaa Education Series

(Elements of Propulsion: Gas Turbines And Rockets (Aiaa Education Series



Elements of Propulsion: Gas Turbines And Rockets
(Aiaa Education Series)
By Jack D. Mattingly
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 867
* Publication Date: 2006-08-30
* ISBN-10 / ASIN: 1563477793
* ISBN-13 / EAN: 9781563477799
Product Description:
This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts: basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners).

Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600 illustrations and pictures show basic concepts, trends, and design examples.

Eight computer programs accompany the text, which allow for rapid calculation of trends, “what if” questions, conceptual design, homework problems, and homework verification. The software runs in the Windows operating system on PC-compatible systems
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Aircraft Propulsion Systems Technology and Design - Aiaa Education Series

Aircraft Propulsion Systems Technology and Design - Aiaa Education Series



Aircraft Propulsion Systems Technology and Design
(Aiaa Education Series)
By Gordon C. Oates
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 528
* Publication Date: 1989-09
* ISBN-10 / ASIN: 093040324X
* ISBN-13 / EAN: 9780930403249

Book Description:
A comprehensive coverage of the key physical concepts that govern gas turbine propulsion systems. Topics include combustion technology, engine/airplane performance matching, inlets and inlet/engine integration, variable convergent/divergent nozzle aerodynamics, and more


File type: RAR
Size: 6622 KB

http://depositfiles.com/files/iqbk6eexj
http://depositfiles.com/files/x0vbhn8gg


 
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Aerothermodynamics of Aircraft Engine Components - Aiaa Education Series

Aerothermodynamics of Aircraft Engine Components - Aiaa Education Series



Aerothermodynamics of Aircraft Engine Components
(Pandora Books)
By Gordon C. Oates
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 551
* Publication Date: 1985-10
* ISBN-10 / ASIN: 0915928973
* ISBN-13 / EAN: 9780915928972
Book Description:
Design and R&D engineers and students will value the comprehensive, meticulous coverage in this volume, which, under the expert editorial supervision of Gordon C. Oates, features the invited work of prominent specialists in aircraft gas turbine engines.
Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design​


http://www.mediafire.com/?mizyoyuijmz

 
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Aerothermodynamics of Gas Turbine Rocket Propulsion, 3rd Ed - Aiaa Education Serie

Aerothermodynamics of Gas Turbine Rocket Propulsion, 3rd Ed - Aiaa Education Serie



Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition (Aiaa Education Series)
By Gordon C. Oates
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 456
* Publication Date: 1997-06
* ISBN-10 / ASIN: 1563472414
* ISBN-13 / EAN: 9781563472411

Book Description:
This seminal book on gas turbine technology has been a best-seller since it was first published in 1984. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are: atmosphere programs, quasi-one-dimensional flows programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and Pc given, Hc and Pc given, isentropic expansion). Used as a standard text in more than 50 universities, the book and software will continue to fulfill the need for a comprehensive modern book on the principles of propulsion.

System Requirements:IBM PC 386/486/586/Pentium or compatible; 640 Kb RAM hard disk with 1.0 Mb of available disk space; EGA or better video capability​

File type: RAR
Size: 5036 KB
كود:
http://mihd.net/rvs7h2
http://rapidshare.com/files/26729736/aerothermodynamics_of_gas_turbine_and_rocket_propulsion.rar
mirror
http://rapidshare.com/files/26738161/Aerothermodynamics_of_Gas_turbine_and_Rocket_propulsion.rar
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Aircraft Engine Design

Aircraft Engine Design



Aircraft Engine Design
(Aiaa Education Series)
By Jack D. Mattingly, William H. Heiser, David T. Pratt
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 692
* Publication Date: 2002-12
* ISBN-10 / ASIN: 1563475383
* ISBN-13 / EAN: 9781563475382


Book Description:
The text presents a complete and realistic aircraft engine design experience. From the request for proposal for a new aircraft to the final engine layout, the book provides the concepts and procedures required for the entire process. It is a significantly expanded and modernized version of the best-selling first edition that emphasizes recent developments impacting engine design such as theta break/throttle ratio, life management, controls, and stealth. The key steps of the process are detailed in 10 chapters that encompass aircraft constraint analysis, aircraft mission analysis, engine parametric (design point) analysis, engine performance (off-design) analysis, engine installation drag and sizing, and the design of inlets, fans, compressors, main combustors, turbines, afterburners, and exhaust nozzles.

The AEDsys software that accompanies the text provides comprehensive computational support for every design step. The software has been carefully integrated with the text to enhance both the learning process and productivity, and allows effortless transfer between British engineering and SI units. The AEDsys software is furnished on CD-ROM and runs in the Windows operating system on PC-compatible systems. A user?s manual is provided with the software, along with the complete data files used for the Air-to-Air Fighter and Global Range Airlifter design examples of the book


File type: RAR
Size: 7867 KB



http://mihd.net/1w2mrz
http://rapidshare.com/files/26736171/aircraft_engine_design.rar
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Hypersonic Airbreathing Propulsion

Hypersonic Airbreathing Propulsion



Hypersonic Airbreathing Propulsion/Book and Disk
(Aiaa Education)
By William H. Heiser, David T. Pratt, Daniel H. Daley, Unmeel B. Mehta
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 587
* Publication Date: 1993-09
* ISBN-10 / ASIN: 1563470357
* ISBN-13 / EAN: 9781563470356
Book Description:
The next great leap for jet propulsion will be to power-sustained, efficient flight through the atmosphere. Hypersonic Airbreathing Propulsion presents the first comprehensive, unified introduction to all elements of the scramjet engine that will make this feat possible.

Developed through course work at the U.S. Air Force Academy, and supported through funding by the NASP program and Wright Laboratory, the text emphasizes fundamental principles, guiding concepts, and analytical derivations and numerical examples having clear, useful, insightful results.

Hypersonic Airbreathing Propulsion is completely self-contained, and comes with HAP software, an extensive array of PC-based, user-friendly computer programs that enable the student to reproduce all results. Based on a great deal of original material, the text includes over 200 figures, five color plates, and 130 homework examples. Physical quantities are expressed in English and SI units throughout

File type: RAR
Size: 7758 KB

http://mihd.net/1fh6i0
hypersonic_airbreathing_propulsion.rar (7.58 MB)
mirror
hypersonic_airbreathing_propulsion.rar (7.58 MB)

Live Links : 2/2Live Links : 2/2
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
(Civil Jet Aircraft Design (Aiaa Education Series

(Civil Jet Aircraft Design (Aiaa Education Series


Civil Jet Aircraft Design (Aiaa Education Series)
By Lloyd R. Jenkinson, Paul Simpkin, Darren Rhodes
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 418
* Publication Date: 1999-09
* ISBN-10 / ASIN: 156347350X
* ISBN-13 / EAN: 9781563473500
Book Description:
This book represents a comprehensive introduction to the modern process of designing transport aircraft from the preliminary stages of conceptual design to detail design of major aircraft components, including cost analysis and optimization. The three authors ensure a balanced presentation, with viewpoints from an educator, a practicing engineer/designer, and an official from the Civil Aviation Authority, U.K.

One of the main objectives of this text is to introduce students to the procedures and practices of civil aircraft design involving conflicting requirements of performance, quality, safety, and environmental issues. The first part of the text deals with the main elements of the preliminary design process for principal aircraft components of a civil transport, including the parametric methods used to define the baseline design configuration. The second part describes the use of spreadsheet methods in aircraft design on four separate design studies.
Co-published with Butterworth-Heinemann

PDF file, 444 pages, 16MB

Civil_Jet_Aircraft_Design.rar (15.78 MB)
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
The Jet Engine- Rolls_Royce

The Jet Engine- Rolls_Royce


Information :
Author : Rolls-Royce engineers | Published by Technical Publications Department, Rolls-Royce, Derby, England | Publication date : 1996 | ISBN : 0902121235 | PDF Format, 292 pages | Original File Size : 20935 KB | Compressed File Size : 19912 KB



Overview :
This book is recognised as the definitive insight into the complex world of gas turbine technology. Written by Rolls-Royce engineers it provides a clear and comprehensive introduction to the workings of the gas turbine.
High–quality and detailed illustrations are featured throughout the book as it takes you on a journey from the theory of jet propulsion to today’s advanced products and provides insights into tomorrow’s technology.
Although primarily aimed at engineers and engineering students, the Jet Engine Book provides a fascinating read for anyone interested in the workings of one of the world’s most complex and technologically demanding products
.​


DOWNLOAD

ویرایش پنجم

http://rapidshare.com/files/174632220/rolls_royce_-_the_jet_engine._5th_edition.pdf

http://www.mediafire.com/file/myxjjtr20ja/Rolls-Royce-The-Jet-Engine-5th-Edition.pdf


Live Links : 1/1
 
آخرین ویرایش:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Rocket and Spacecraft Propulsion: Principles, Practice and New Developments

Rocket and Spacecraft Propulsion: Principles, Practice and New Developments



# Publisher: Springer
# Number Of Pages: 344
# Publication Date: 2004-11-23
# ISBN / ASIN: 3540221905

Book Description:
The revised edition of this practical, hands-on book discusses the range of launch vehicles in use today throughout the world, and includes the very latest details of some of the advanced propulsion systems currently being developed. The author covers the fundamentals of the subject, from the basic principles of rocket propulsion and vehicle dynamics through the theory and practice of liquid and solid propellant motors, to new and future developments. The revised edition will stick to the same principle of providing a serious exposition of the principles and practice of rocket propulsion, but from the point of view of the user and enquirer who is not an engineering specialist. Most chapters will remain substantially the same as the first edition; they will be updated where necessary and errata corrected. The main revisions will be to the chapter on electric propulsion where there have been significant new developments both in engine types and in practical applications. This is now seen as the key to planetary exploration by robotic probes and should therefore be reflected. Nuclear propulsion has emerged from the doldrums and is now seen as a definite possibility for outer solar system robotic exploration; and as enabling technology for a human mars expedition. A new chapter on nuclear thermal propulsion has been added to reflect this revival of interest

vector PDF file (not scan), size 13MB
RAR archive password: gigapedia.org

http://w15.easy-share.com/6730341.html
or
3540221905.rar (12 MB)
or
http://www.icefile.com/index.php?page=main&id=25cb8352&name=3540221905.rar
or
http://www.icefile.com/index.php?page=main&id=25cb8352&name=3540221905.rar
Live Links : 1/1Live Links : 1/1
 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Future Spacecraft Propulsion Systems

Future Spacecraft Propulsion Systems




Future Spacecraft Propulsion Systems: Enabling Technologies for Space Exploration (Springer Praxis Books / Astronautical Engineering)
By Paul A. Czysz,&nbspClaudio Bruno,

* Publisher: Springer
* Number Of Pages: 496
* Publication Date: 2006-02-10
* ISBN / ASIN: 3540231617

Book Description:
In Future Spacecraft Propulsion Systems the authors demonstrate the need to break free from the old established concepts of expendable rockets, using chemical propulsion, and to develop new breeds of launch vehicle capable of both launching payloads into orbit at dramatically reduced cost, and for sustained operations in low-Earth orbit. The next steps, they explain, to establishing a permanent "presence" in the solar system beyond Earth are the commercialisation of sustained operations on the Moon, and the development of advanced nuclear or high-energy space propulsion systems for solar system exploration out to the boundary of interstellar space. In the future, high-energy particle research facilities may one day yield a very high-energy propulsion system that will take us to the nearby stars, or even beyond. This is a timely and comprehensive book, putting spacecraft propulsion systems in perspective


PDF file (not scan), size 9.5MB
RAR archive

http://www.4shared.com/file/54693377/f7ca3bbd/Future_Spacecraft_Propulsion_Systems.html
 

سـعید

مدیر بازنشسته
Rocket and Spacecraft Propulsion - Principles, Practice and New Developments

Rocket and Spacecraft Propulsion - Principles, Practice and New Developments

Rocket and Spacecraft Propulsion - Principles, Practice and New Developments



Size: 12,679 KB



 

سـعید

مدیر بازنشسته
Gas Turbine Theory, Fourth Edition



Author(s): Henry Cohen, G. F. C. Rogers, H. I. H. Saravanamuttoo
Publisher: Addison Wesley Longman
Date : 2005
Pages : 442
Format : PDF
OCR : Y
Quality : good
Language : English
ISBN-10 : 0582236320

http://rapidshare.com/files/234259015/0582236320.rar | 8520 KB
 

سـعید

مدیر بازنشسته
Principles of Jet Propulsion and Gas Turbines



Author(s): Maurice Joseph Zucrow
Publisher: John Wiley & Sons
Date : 1948
Pages : 563
Format : PDF
OCR : N
Quality : good
Language : English
ISBN-10 : 7852123456

http://rapidshare.com/files/234260358/zucrow.rar | 11994 KB
 

سـعید

مدیر بازنشسته
Rocket Propulsion Elements, 7th Edition free download

http://www.freebookspot.in/upload/Aeronautical Engineering/Rocket_Propulsion_Elements__7th_Edition_19.11.2008_0_00_00.jpg

Author(s): George P. Sutton Oscar Biblarz
Publisher: Wiley-Interscience
Date : PDF
Pages : 751
Format : PDF
OCR : Y
Quality : good
Language : English
ISBN-10 : 0471326429

http://rapidshare.com/files/225588149/sutton-biblarz_-_rocket_propulsion_elements.rar
 
آخرین ویرایش توسط مدیر:

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Gas Turbine Engines for Model Aircraft

Gas Turbine Engines for Model Aircraft




Gas Turbine Engines for Model Aircraft By Kurt Schreckling
Publisher: Traplet Publications Ltd 2003 | 88 Pages | ISBN: 1951058916 | DJVU | 5 MB



Aturbo-jet engine for model aircraft? What's a turbo-jet, anyway? "What sort of engine have you got in there, then?" These are the questions I have heard so often, even from experienced power modellers. Sometimes a little more knowledge was betrayed by the question: "How many turbine wheels has it got?" Occasionally — very occasionally - I would be asked a question on the compression ratio. Then I knew that J was in the presence of a real expert! But all my interrogators had one thing in common: they all wanted to know exactly how this jet turbine device worked.
A turbo-jet, also known as a jet turbine engine, exploits a gas turbine to produce thrust. It is called a gas turbine because the working medium - air - is in a gaseous form. Please note that this has nothing to do with the possibility of using fuel in a gaseous state. In its simplest constructional form this type of heat engine makes a high-performance power source for an air­craft. The gas turbine becomes a jet turbine, or turbo-jet, when the usable energy in the exhaust gas from the turbine is concen­trated using a nozzle, or jet. However, this is not essential in principle.
The first aircraft propelled by a jet turbine was the He 178, which flew for the first time on 22.8.1939. It was The first experimental design, ai built in the Heinkel factory constructed using simple means and the pilot was Erich completed in April 1989 and ran Warsitz. This revolutionary engine was the creation of Dr. Papst von Ohain. On its very first flight this air­craft - the first ever to be powered by a turbo-jet engine - reached a speed of 600 km/hr, faster than any other series-produced airscrew-driven aircraft of the time. In the truest sense of the phrase the engine was simple and ingenious: a single com­pressor wheel sucked the air in and compressed it in the combustion chamber.



letitbit
uploading
sharingmatrix
depositfiles
megaupload

 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار
Gas Turbine Theory, Fourth Edition

Gas Turbine Theory, Fourth Edition




Gas Turbine Theory, Fourth Edition
Prentice Hall | June 10, 2001 | ISBN-10: 013015847X | 512 pages | DJvu | 4.2 mb

This is the 50th Anniversary edition of this established title. This text places the theory of gas turbines in the context of the practical realities facing aerospace, mechanical, and industrial designers. There is a strong emphasis on describing the physical reasons for solutions to design problems using practical examples. When the First Edition of this book was written in 1951, the gas turbine was just becoming established as a powerplant for military aircraft. It took another decade before the gas turbine was introduced to civil aircraft, and this market developed so rapidly that the ocean liner was rendered obsolete. Other markets like naval propulsion, pipeline compression and electrical power applications grew steadily. In recent years the gas turbine, in combination with the steam turbine, has played an ever-increasing role in power generation. Despite the rapid advances in both output and efficiency, the basic theory of the gas turbine has remained unchanged. The layout of this new fifth edition is broadly similar to the original, but greatly expanded and updated, comprising an outline of the basic theory, aerodynamic design of individual components, and the prediction of off-design performance. Descriptions of engine developments and current markets make this book useful to both students and practising engineers.


Download

mirror

 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار




Philip P. Walsh / Paul Fletcher, «Gas Turbine Performance»
Blackwell Science | ISBN 063206434X | 2nd edition (October 30, 2004) | PDF | 5 Mb | 646 pages


Synopsis:

This book provides a practical guide to the fundamentals of performance, including the requirements of all major applications: power generation, mechanical drive, automotive, marine and aircraft installations. The new edition includes two additional chapters on performance issues of engines in-service and on the techno-economic issues that determine whether a gas turbine project will be profitable.



Table of Contents

Foreword to the first edition
Preface
Gas turbine engine configurations 1
1 Gas turbine engine applications 9
2 The operational envelope 61
3 Properties and charts for dry air, combustion products and other working fluids 102
4 Dimensionless, quasidimensionless, referred and scaling parameter groups 143
5 Gas turbine engine components 159
6 Design point performance and engine concept design 292
7 Off design performance 383
8 Transient performance 444
9 Starting 477
10 Windmilling 501
11 Engine performance testing 519
12 The effects of water - liquid, steam and ice 564
13 Fuel and oil properties and their impact 587
14 Performance of in-service products 599
15 Performance and the economics of gas turbine engines 607
App. A Station numbering and nomenclature 617
App. B: Unit conversions 625
Index 631



DOWNLOAD FROM:
http://rapidshare.com/files/170232404/Gas_Turbine_Performance.rar
Edit Del

or

http://rapidshare.com/files/47523445/Gas_Turbine_Performance.pdf


 

Sparrow

مدیر تالار مهندسی هوافضا
مدیر تالار

J. Seddon, E. L. Goldsmith
American Institute of Aeronautics and Astronautics, 1999 - Science - 407 pages
"Intake Aerodynamics, Second Edition" presents computational advancements and discoveries in intake aerodynamics. A companion volume to "Practical Intake Aerodynamic Design," this important text considers the problem of airflow, both internal and external to air intake, as applied to civil and military aircraft. It covers the aerodynamics of subsonic and supersonic intakes in real flows, maintaining a progression through the transonic range. Also considered is the joint perspective of the airframe designer and the propulsion specialist in practical cases.
Readers will gain insight into the fluid mechanics behind the deceleration of air from free stream to engine velocity, and an understanding of air compression and external drag in extensively revised chapters reflecting progress in the field. More than 300 drawings and diagrams help to illustrate the points defined throughout the book.
Copublished with Blackwell Science Ltd. Outside the United States and Canada, order from Blackwell Science Ltd., United Kingdom, tel 44 1865 206 206.





 

پیوست ها

  • Intake Aerodynamics.rar
    5.8 مگایابت · بازدیدها: 0
وضعیت
موضوع بسته شده است.
بالا