Boeing 747

One of the adavnced commerical airliner.

Boeing 747

One of the adavnced commerical airliner.

B-2 bomber

The most expensive aircraft and bomber ever built.

F-22 raptor

The most advanced fighter jet in world and stealth aircraft ever gone into production.

An-225 mirya

The world largest aircraft only one of its kind ,intially for buran spaceplane transport.

World largest aircraft carrier

Hold a speed of 35 knots and carries 90+ aircraft.

MI mi-26

The most heavy weight lifting helicopter of lifyting weight 13T.

Soyuz rocket

The oldest and most frequent launched rocket efficent liq proplled .

Wednesday, February 12, 2014

Introduction to Finite Elements in Engineering by Tirupathi R. Chandrupatla

Introduction to Finite Elements in Engineering by Tirupathi R. Chandrupatla


The first edition of this book appeared over 10 years ago and the second edition followed a few years later. We received positive feedback from professors who taught from the book and from students and practicing engineers who used the book. We also benefited from the feedback received from the students in our courses for the past 20 years. We have incorporated several suggestions in this edition. The underlying philosophy of the book is to provide a clear presentation of theory, modeling, and implementation into computer programs. The pedagogy of earlier editions has been retained in this edition.
New material has been introduced in several chapters. Worked examples and exercise problems have been added to supplement the learning process. Exercise problems stress both fundamental understanding and practical considerations. Theory and computer programs have been added to cover acoustics, axisymmetric quadrilateral elements, conjugate gradient approach, and eigenvalue evaluation. Three additional programs have now been introduced in this edition. All the programs have been developed to work in the Windows environment. The programs have a common structure that should enable the users to follow the development easily. The programs have been provided in Visual Basic, Microsoft Excel/Visual Basic, MATLAB, together with those provided earlier in QBASIC, FORTRAN and C. The Solutions Manual has also been updated.


Rocket Propulsion Elements by George P. Sutton and Oscar Biblarz

Rocket Propulsion Elements by George P. Sutton and Oscar Biblarz

the definitive text on rocket propulsion—now revised to reflect advancements in the field For sixty years, Sutton′s Rocket Propulsion Elements has been regarded as the single most authoritative sourcebook on rocket propulsion technology. As with the previous edition, coauthored with Oscar Biblarz, the Eighth Edition of Rocket Propulsion Elements offers a thorough introduction to basic principles of rocket propulsion for guided missiles, space flight, or satellite flight. It describes the physical mechanisms and designs for various types of rockets′ and provides an understanding of how rocket propulsion is applied to flying vehicles. Updated and strengthened throughout, the Eighth Edition explores: The fundamentals of rocket propulsion, its essential technologies, and its key design rationale The various types of rocket propulsion systems, physical phenomena, and essential relationships The latest advances in the field such as changes in materials, systems design, propellants, applications, and manufacturing technologies, with a separate new chapter devoted to turbopumps Liquid propellant rocket engines and solid propellant rocket motors, the two most prevalent of the rocket propulsion systems, with in–depth consideration of advances in hybrid rockets and electrical space propulsion Comprehensive and coherently organized, this seminal text guides readers evenhandedly through the complex factors that shape rocket propulsion, with both theory and practical design considerations. Professional engineers in the aerospace and defense industries as well as students in mechanical and aerospace engineering will find this updated classic indispensable for its scope of coverage and utility 






The Finite Element Method in Engineering by Singiresu S. RAO

The Finite Element Method in Engineering by Singiresu S. RAO 

Finite Element Analysis is an analytical engineering tool originated by the Aerospace and nuclear power industries to find usable, approximate solutions to problems with many complex variables. It is an extension of derivative and integral calculus, and uses very large matrix arrays and mesh diagrams to calculate stress points, movement of loads and forces, and other basic physical behaviors. Rao provides a thorough grounding of the mathematical principles for setting up finite element solutions in civil, mechanical, and aerospace engineering applications. The new edition includes examples using modern computer tools such as Matlab, Ansys, Nastran, and Abaqus. 

Professional engineers will benefit from the introduction to the many useful applications of finite element analysis, and will gain a better understanding of its limitations and special uses. 
New to this edition: Examples and applications in Matlab, Ansys, and Abaqus Structured problem solving approach in all worked examples New discussions throughout, including the direct method of deriving finite element equations, use of strong and weak form formulations, complete treatment of dynamic analysis, and detailed analysis of heat transfer problems
More examples and exercises All figures revised and redrawn for clarity


                                                                  


Rocket and Spacecraft Propulsion: Principles by Martin J. L. Turner


Rocket and Spacecraft Propulsion: Principles by Martin J. L. Turner


"Turner (Univ. of Leicester, UK) offers an updated version of his 2000 book. … He examines rockets and rocket engines from the viewpoint of physical principles and gives accessible explanations on how rockets work. … Turner uses graphs to help interpret many equations. … Summing Up: Recommended. Upper-division undergraduates; graduate students." (D.B. Mason, CHOICE, Vol. 42 (10), June, 2005)
"As a rule, textbooks have equations and other books have colour photographs, but this book breaks that rule by including both. Its centre-section of 20 colour plates certainly sets it apart from most textbooks … . there is plenty of information between the equations to engage anyone with an interest in the technology. It also has a number of appendices and a five-page index. … The book is usefully up to date in its coverage. … This book remains an excellent primer on the principles of rocket propulsion." (Mark Williamson, International Space Review, 2005)
The revised edition of this practical, hands-on book discusses the launch vehicles in use today throughout the world, and includes the latest details on advanced systems being developed, such as electric and nuclear propulsion.
The author covers the fundamentals, 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.
He provides a serious exposition of the principles and practice of rocket propulsion, from the point of view of the user who is not an engineering specialist. 



Aircraft Conceptual Design Synthesis by denis howe

Aircraft Conceptual Design Synthesis by denis howe



Aircraft Conceptual Design Synthesis means design by fitness-for-purpose. Design engineers can jump off from the point of given parameters and requirements – required performance, payloads and other factors.
This is the first book for the aeronautical designer devoted to guiding the reader through this highly effective conceptual design synthesis process. This forms the procedure for the initial stage of the aircraft design process – the interpretation of a requirement into the preliminary layout. A logical design sequence is developed utilizing original modules to represent propulsion, lift, drag, mass, and performance. Aircraft Conceptual Design Synthesis includes a disk of spreadsheets that provides core data. Unlike existing approaches, the design synthesis method can be applied to novel aircraft concepts.
CONTENTS INCLUDE
  • The design process
  • Aircraft configuration
  • Flight regime and powerplant considerations
  • Fuselage layout
  • Configuration of the wing
  • Basic lift, drag and mass representations
  • Performance estimation
  • Parametric analysis and optimisation
  • Analysis of concept design 


                                                                           



Tuesday, February 11, 2014

Aircraft Design: A Conceptual Approach by Daniel P. Raymer

Aircraft Design: A Conceptual Approach  by Daniel P. Raymer

This best-selling textbook presents the entire process of aircraft conceptual design - from requirements definition to initial sizing, configuration layout, analysis, sizing, optimization, and trade studies. Widely used in industry and government aircraft design groups, "Aircraft Design: A Conceptual Approach" is also the design text at major universities around the world. A virtual encyclopedia of engineering, it is known for it's completeness, easy-to-read style, and real-world approach to the process of design. Special features: more than 900 pages of design methods, illustrations, tips, explanations, and equations; overviews of lofting, subsystems, maintainability, producibility, vulnerability, and stealth; concepts and calculation methods for aerodynamics, stability and control, propulsion, structures, weights, performance, and cost; coverage of conventional and unconventional design methods, including UAV, canard, tandem wing, C-wing, oblique wing, asymmetrical, multi-fuselage, wing-in-ground-effect, and more; and, VTOL, helicopter, spacecraft, launch vehicle, hypersonic, and airship design. New topics include: advice on how to become an aircraft designer; electric aircraft, batteries, fuel cells, and solar cells; green airplanes, including biofuels, GTL, hydrogen, methane, and nuclear; active aeroelastic wing and advanced tailless concepts; and enhanced learning materials, including chapter opening summaries with set-the-stage art, descriptive sidebar definitions and tips, and what-we-learned chapter       

                                                                           


Wednesday, December 25, 2013

Computational Fluid Dynamics- The Basics with Applications by Anderson J.D.Jr

 Computational Fluid Dynamics- The Basics with Applications by Anderson J.D.Jr



The Beginner's guide to Computational Fluid Dynamics From aerospace design to applications in civil, mechanical, and chemical engineering, computational fluid dynamics (CFD) is as essential as it is complex. The most accessible introduction of its kind, Computational Fluid Dynamics: The Basics With Applications, by experienced aerospace engineer John D. Anderson, Jr., gives you a thorough grounding in: the governing equations of fluid dynamics--their derivation, physical meaning, and most relevant forms; numerical discretization of the governing equations--including grids with appropriate transformations and popular techniques for solving flow problems; common CFD computer graphic techiniques; applications of CFD to 4 classic fluid dynamics problems--quasi-one-dimensional nozzle flows, two-dimensional supersonic flow, incompressible couette flow, and supersonic flow over a flat plate; state-of-the-art algorithms and applications in CFD--from the Beam and Warming Method to Second-Order Upwind Schemes and beyond.

                                     


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