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Author : Earl Arthur Thornton
Publisher : AIAA
Page : 508 pages
File Size : 48,5 Mb
Release : 1996
Category : Aerothermodynamics
ISBN : 1600861261
Author : Earl Arthur Thornton
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 576 pages
File Size : 55,7 Mb
Release : 1992
Category : Science
ISBN : UOM:39015028414509
This text presents recent research and development in aerothermodynamics, advanced light metals and composites, thermal structures, materials performance and failure criteria, and intelligent processing of materials, as they relate to high-speed flight. Researchers and designers of aerospace vehicles for high-speed flight, as well as materials scientists, should find this text valuable.
Author : Earl A. Thornton
Publisher : Unknown
Page : 128 pages
File Size : 41,9 Mb
Release : 1995
Category : Electronic
ISBN : 1600866360
Author : Earl Arthur Thornton
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 432 pages
File Size : 43,6 Mb
Release : 1995
Category : Science
ISBN : UOM:39015034518848
Presenting recent advances in technology for high-temperature structures and materials, this book should be of interest to engineers and material scientists working on advanced aeronautics and astronautics projects that involve elevated temperatures. Other topics dicussed include high-speed flight in the atmosphere, propulsion systems, and orbiting spacecraft.
Author : Earl A. Thornton
Publisher : AIAA
Page : 430 pages
File Size : 44,8 Mb
Release : 1995
Category : Aerothermodynamics
ISBN : 1600864171
Author : Bengt Sundén,Juan Fu
Publisher : Academic Press
Page : 272 pages
File Size : 45,6 Mb
Release : 2016-10-19
Category : Technology & Engineering
ISBN : 9780128097618
Heat Transfer in Aerospace Applications is the first book to provide an overall description of various heat transfer issues of relevance for aerospace applications. The book contains chapters relating to convection cooling, heat pipes, ablation, heat transfer at high velocity, low pressure and microgravity, aircraft heat exchangers, fuel cells, and cryogenic cooling systems. Chapters specific to low density heat transfer (4) and microgravity heat transfer (9) are newer subjects which have not been previously covered. The book takes a basic engineering approach by including correlations and examples that an engineer needs during the initial phases of vehicle design or to quickly analyze and solve a specific problem. Designed for mechanical, chemical, and aerospace engineers in research institutes, companies, and consulting firms, this book is an invaluable resource for the latest on aerospace heat transfer engineering and research. Provides an overall description of heat transfer issues of relevance for aerospace applications Discusses why thermal problems arise and introduces the various heat transfer modes Helps solve the problem of selecting and calculating the cooling system, the heat exchanger, and heat protection Features a collection of problems in which the methods presented in the book can be used to solve these problems
Author : Sergio Pellegrino,Simon D. Guest
Publisher : Springer Science & Business Media
Page : 503 pages
File Size : 43,9 Mb
Release : 2013-03-09
Category : Science
ISBN : 9789401595148
This collection presents 49 contributions by engineers, architects, biologists, and applied mathematicians interested in deployable structures. Aerospace structures are currently at the leading edge, and this is reflected by a larger number of contributions covering the full spectrum of concepts, simulations, testing, and working systems.
Author : Mark Ahlers
Publisher : SAE International
Page : 117 pages
File Size : 49,9 Mb
Release : 2016-03-02
Category : Science
ISBN : 9780768083033
The simultaneous operation of all systems generating, moving, or removing heat on an aircraft is simulated using integrated analysis which is called Integrated Energy System Analysis (IESA) for this book. Its purpose is to understand, optimize, and validate more efficient system architectures for removing or harvesting the increasing amounts of waste heat generated in commercial and military aircraft. In the commercial aircraft industry IESA is driven by the desire to minimize airplane operating costs associated with increased system weight, power consumption, drag, and lost revenue as cargo space is devoted to expanded cooling systems. In military aircraft thermal IESA is also considered to be a key enabler for the successful implementation of the next generation jet fighter weapons systems and countermeasures. This book contains a selection of papers relevant to aircraft thermal management IESA published by SAE International. They cover both recently developed government and industry- funded thermal management IESA such as the Integrated Vehicle Energy Technology (INVENT) program, and older published papers still relevant today which address modeling approaches.
Author : Dora Musielak
Publisher : John Wiley & Sons
Page : 516 pages
File Size : 45,7 Mb
Release : 2023-01-10
Category : Technology & Engineering
ISBN : 9781119640608
Scramjet Propulsion Explore the cutting edge of HAP technologies with this comprehensive resource from an international leader in her field Scramjet Propulsion: A Practical Introduction delivers a comprehensive treatment of hypersonic air breathing propulsion and its applications. The book covers the most up-to-date hypersonic technologies, like endothermic fuels, fuel injection and flameholding systems, high temperature materials, and TPS, and offers technological overviews of hypersonic flight platforms like the X-43A, X-51A, and HiFIRE. It is organized around easy-to-understand explanations of technical challenges and provides extensive references for the information contained within. The highly accomplished author provides readers with a fulsome description of the theoretical underpinnings of hypersonic technologies, as well as critical design and technology issues affecting hypersonic air breathing propulsion technologies. The book’s combination of introductory theory and advanced instruction about individual hypersonic engine components is ideal for students and practitioners in fields as diverse as hypersonic vehicle and propulsion development for missile defense technologies, launch aerospaceplanes, and civilian transports. Over 250 illustrations and tables round out the material. Readers will also learn from: A thorough introduction to hypersonic flight, hypersonic vehicle concepts, and a review of fundamental principles in hypersonic air breathing propulsion Explorations of the aerothermodynamics of scramjet engines and the design of scramjet components, as well as hypersonic air breathing propulsion combustors and fuels Analyses of dual-mode combustion phenomena, materials structures, and thermal management in hypersonic vehicles, and combined cycle propulsion An examination of CFD analysis, ground and flight testing, and simulation Perfect for researchers and graduate students in aerospace engineering, Scramjet Propulsion: A Practical Introduction is also an indispensable addition to the libraries of engineers working on hypersonic vehicle development seeking a state-of-the-art resource in one of the most potentially disruptive areas of aerospace research today.
Author : Simon Appel,Jaap Wijker
Publisher : Springer Nature
Page : 399 pages
File Size : 44,7 Mb
Release : 2021-08-31
Category : Technology & Engineering
ISBN : 9783030789992
This book provides recommendations for thermal and structural modelling of spacecraft structures for predicting thermoelastic responses. It touches upon the related aspects of the finite element and thermal lumped parameter method. A mix of theoretical and practical examples supports the modelling guidelines. Starting from the system needs of instruments of spacecraft, the reader is supported with the development of the practical requirements for the joint development of the thermal and structural models. It provides points of attention and suggestions to check the quality of the models. The temperature mapping problem, typical for spacecraft thermoelastic analysis, is addressed. The principles of various temperature mapping methods are presented. The prescribed average temperature method, co-developed by the authors, is discussed in detail together with its spin-off to provide high quality conductors for thermal models. The book concludes with the discussion of the application of uncertainty assessment methods. The thermoelastic analysis chain is computationally expensive. Therefore, the 2k+1 point estimate method of Rosenblueth is presented as an alternative for the Monte Carlo Simuation method, bringing stochastic uncertainty analysis in reach for large thermoelastic problems.
Author : Zhenhan Yao,Mingwu Yuan
Publisher : Springer Science & Business Media
Page : 354 pages
File Size : 52,8 Mb
Release : 2007-12-31
Category : Technology & Engineering
ISBN : 9783540482604
Here are the printed proceedings of EPMESC X, held on August 21-23, 2006 in Sanya, Hainan Island of China. It includes 14 full papers of plenary and semi-plenary lectures and approximately 166 one-page summaries. The accompanying CD-ROM includes all 180 full papers presented at the conference.
Author : Anonim
Publisher : Unknown
Page : 492 pages
File Size : 46,7 Mb
Release : 1997
Category : Astrodynamics
ISBN : PSU:000031334518
Author : John P. Lynch
Publisher : Unknown
Page : 552 pages
File Size : 49,8 Mb
Release : 1999
Category : Space stations
ISBN : NASA:31769000473937
Author : Jorge Colman Lerner,Ulfilas Boldes
Publisher : BoD – Books on Demand
Page : 728 pages
File Size : 46,9 Mb
Release : 2011-07-27
Category : Science
ISBN : 9789533076232
The book "Wind Tunnels and Experimental Fluid Dynamics Research" is comprised of 33 chapters divided in five sections. The first 12 chapters discuss wind tunnel facilities and experiments in incompressible flow, while the next seven chapters deal with building dynamics, flow control and fluid mechanics. Third section of the book is dedicated to chapters discussing aerodynamic field measurements and real full scale analysis (chapters 20-22). Chapters in the last two sections deal with turbulent structure analysis (chapters 23-25) and wind tunnels in compressible flow (chapters 26-33). Contributions from a large number of international experts make this publication a highly valuable resource in wind tunnels and fluid dynamics field of research.
Author : Naotake Noda
Publisher : Routledge
Page : 211 pages
File Size : 53,8 Mb
Release : 2018-05-04
Category : Science
ISBN : 9781351408400
Thermal Stresses, 2nd Edition is the first book comprehensive volume on thermal stresses. It provides a sound grounding in the fundamental theory of thermal stresses as well as includes a multitude of applications. Many solved examples are included in the text, with numerous problems at the end of each chapter.The book starts with an introduction to the elementary theory, at the undergraduate level, and then progresses with the exposition of more advanced methods. The authors introduce the topics in a clear fashion, easy to grasp by students, engineers and scientists.
