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Title Structural Loads Analysis for Commercial Transport Aircraft
Author Ted L. Lomax
Publisher AIAA (American Institute of Aeronautics & Astronautics)
Release 1996
Category Science
Total Pages 280
ISBN
Language English, Spanish, and French
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Book Summary:

This important text covers all aspects of structural loads analysis and provides some continuity between what was done on earlier airplane designs and what the current applications of the present regulations require.

Structural Loads Analysis by Ted L. Lomax

Title Structural Loads Analysis
Author Ted L. Lomax
Publisher AIAA
Release 1996
Category Airframes
Total Pages 297
ISBN 9781600861185
Language English, Spanish, and French
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Title Influence of flight control laws on structural sizing of commercial aircraft
Author Rahmetalla Nazzeri
Publisher Cuvillier Verlag
Release 2021-11-15
Category Technology & Engineering
Total Pages 180
ISBN 3736965168
Language English, Spanish, and French
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Book Summary:

The increasing demand for new civil aircraft pushes aircraft manufacturers to develop innovative solutions that lead in particular to mass reductions. One way to achieve these kinds of improvements is the use of multidisciplinary analysis and optimization. In this sense the intention of this PhD thesis is to develop a multidisciplinary framework in order to quantify the impact of load alleviation function parameter changes on structural components like the wing and fuselage in terms of resulting mass changes. The developed iterative process chain covers the loads calculation including an active load alleviation system, a structural assessment of the wing and fuselage components and a dedicated feedback loop in order to update mass and stiffness properties of the loads calculation model. The study shows that significant mass reductions are achievable while on the other hand estimated mass penalties are irrelevant.

Title The Proceedings of the 2018 Asia Pacific International Symposium on Aerospace Technology APISAT 2018
Author Xinguo Zhang
Publisher Springer
Release 2019-06-08
Category Technology & Engineering
Total Pages 3068
ISBN 981133305X
Language English, Spanish, and French
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Book Summary:

This book is a compilation of peer-reviewed papers from the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018). The symposium is a common endeavour between the four national aerospace societies in China, Australia, Korea and Japan, namely, the Chinese Society of Aeronautics and Astronautics (CSAA), Royal Aeronautical Society Australian Division (RAeS Australian Division), the Korean Society for Aeronautical and Space Sciences (KSAS) and the Japan Society for Aeronautical and Space Sciences (JSASS). APISAT is an annual event initiated in 2009 to provide an opportunity for researchers and engineers from Asia-Pacific countries to discuss current and future advanced topics in aeronautical and space engineering.

Title Introduction to Aircraft Aeroelasticity and Loads
Author Jan R. Wright
Publisher John Wiley & Sons
Release 2015-02-23
Category Technology & Engineering
Total Pages 574
ISBN 1118488016
Language English, Spanish, and French
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Book Summary:

As an introduction to aircraft aero elasticity and dynamic loads, this book will not only be welcomed by junior practitioners in industry and graduate students, it will also form an excellent basis for several university courses on aero elasticity.

Title Preliminary Design of Graphite Composite Wing Panels for Commercial Transport Aircraft
Author
Publisher
Release 1980
Category
Total Pages 68
ISBN
Language English, Spanish, and French
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Book Summary:

This commercial aircraft wing surface panel configuration study subjectively assessed practical and producible graphite/epoxy designs. Key experienced engineering, manufacturing, and quality control personnel provided the assessment information, using definitive data as well as their experience and judgement in screening and selection of the final panel configuration. A multilevel screening procedure was used to review the panel designs, considering the following areas: (1) Structural functions; (2) Efficiency; (3) Manufacturing and producibility; (4) Costs; (5) Maintainability; and (6) Inspectability As each progressive screening level was reviewed, more definitive information on the structural efficiency (weight), manufacturing, and inspection procedures was established to support the design selection. The final design selection represents a reasonable compromise between all requirements.

Title Introduction to Aircraft Aeroelasticity and Loads
Author Jan Robert Wright
Publisher John Wiley & Sons
Release 2008-02-08
Category Technology & Engineering
Total Pages 524
ISBN 0470858400
Language English, Spanish, and French
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Book Summary:

Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques. Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift. Includes up-to-date experimental methods and analysis. Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.

Title New Results in Numerical and Experimental Fluid Mechanics XIII
Author Andreas Dillmann
Publisher Springer Nature
Release 2021
Category Aerodynamics
Total Pages 787
ISBN 3030795616
Language English, Spanish, and French
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Book Summary:

This book offers timely insights into research on numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications. It reports on findings by members of the STAB (German Aerospace Aerodynamics Association) and DGLR (German Society for Aeronautics and Astronautics) and covers both nationally and EC-funded projects. Continuing on the tradition of the previous volumes, the book highlights innovative solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike. .

Title Structural Dynamics in Aeronautical Engineering
Author Maher N. Bismarck-Nasr
Publisher AIAA
Release 1999
Category Airframes
Total Pages 293
ISBN 9781600861178
Language English, Spanish, and French
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Book Summary:

Annotation "Structural Dynamics in Aeronautical Engineering is a comprehensive introduction to the modern methods of dynamic analysis of aeronautical structures. The text represents carefully developed course materials, beginning with an introductory chapter on matrix algebra and methods for numerical computations, followed by a series of chapters discussing specific aeronautical applications. In this way, the student can be guided from the simple concept of a single-degree-of-freedom structural system to the more complex multidegree-of-freedom and continuous systems, including random vibrations, nonlinear systems, and aeroelastic phenomena. Among the various examples used in the text, the chapter on aeroelasticity of flight vehicles is particularly noteworthy with its clear presentation of the phenomena and its mathematical formulation for structural and aerodynamic loads.

Title An Introduction to Aircraft Performance
Author Mario Asselin
Publisher AIAA
Release 1997
Category Airplanes
Total Pages 354
ISBN 9781600860249
Language English, Spanish, and French
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Book Summary:

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