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AERO 3-2 BOOKS

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COMPUTATIONAL AERODYNAMICS:

Computational Fluid Dynamics- The Basics with Applications, By Anderson, J.D., Jr.
McGraw-Hill Inc.,1995


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.


Computational Fluid Mechanics and Heat Transfer, By Anderson, D.A., Tannehill, J.C., Pletcher, R.H.
Second Edition, Taylor and Francis, 1997


This comprehensive text provides basic fundamentals of computational theory and computational methods. The book is divided into two parts. The first part covers material fundamental to the understanding and application of finite-difference methods. The second part illustrates the use of such methods in solving different types of complex problems encountered in fluid mechanics and heat transfer. The book is replete with worked examples and problems provided at the end of each chapter.

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CONCEPTUAL DESIGN OF FLIGHT VEHICLES:

Aircraft Design: A Conceptual Approach By Raymer, D.P.
3rd edn., AIAA Education Series, AIAA,1999.
ISBN: 1-56347-281-0.

Winner of the Summerfield Book Award, winner of the Aviation-Space Writers Association Award of Excellence, and with over 30,000 copies sold, this is consistently the top-selling AIAA textbook title. This highly regarded textbook presents the entire process of aircraft conceptual design - from requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studies - in the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 900 pages of design methods, illustrations, tips, explanations, and equations, and has extensive appendices with key data essential to design. The book is the required design text at numerous universities around the world and is a favorite of practicing design engineers. The new fourth edition is enhanced in many areas, with improvements and reworking of the text, expanded sizing and analysis methods, and up-to-date treatments of emerging technologies and concepts. A new section provides an introduction to spaceflight and rockets including thrust analysis and vehicle sizing for launch and planetary missions. Appendices are revised and additional exam questions are provided.

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Aircraft Conceptual Design Synthesis By Howe, D.
Professional Engineering Publishing, London,2000.
ISBN: 1-86058-301-6.


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.

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Introduction to Aircraft Design By Fielding,
J.P.Cambridge University Press, 2005,
ISBN: 0-521-657222-9.

AEROSPACE VEHICLE PROPULSION- II

Rocket Propulsion Elements By Sutton, G.P. and Biblarz, O.
7th edn., Wiley, 2001,
ISBN: 0-471-32642-9


For professional engineers in the aerospace and defense industries as well as undergraduate and graduate students in mechanical and aerospace engineering, this time-honored resource is indispensable for its scope of coverage and utility.

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Rocket and Spacecraft Propulsion By Turner, M.J.L.
2nd edn., Springer, 2005.
ISBN: 3-540-22190.


Space exploration and research depends fundamentally on the use of rockets to launch probes and manned vehicles beyond the earths atmosphere. The first successful launch vehicles were developed in the 1960s from concepts dating back to the 1930s.
This practical book written from the perspective of the space scientist deals with the latest applications and propulsion concepts at a level readable by space scientists and students without a formal engineering background.
There are seven main topics: Principles of rocket propulsion and base vehicle dynamics; Thermal motors and the thermodynamics of thrust; Liquid propellant motors; Solid propellant motors; Launch vehicles, station keeping and attitude control, interplanetary transfer vehicles and dynamics; New developments: advanced thermal motors; electric propulsion and dynamics of electrically propelled vehicles; Future developments, fission and fusion powered propulsion.