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Introduction to Aircraft Aeroelasticity and Loads

Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some more advanced methodologies. Finally, it explains how industrial certification requirement.

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http://schema.org/alternateName

  • "飞机气动弹性力学及载荷导论"
  • "Fei ji qi dong dan xing li xue ji zai he dao lun"
  • "Introduction to aircraft aeroelasticity and loads"

http://schema.org/description

  • "Introduction to Aircraft aeroelasticity and Loads, SecondEdition is an updated new edition offering comprehensivecoverage of the main principles of aircraft aeroelasticity andloads. For ease of reference, the book is divided into three partsand begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control, and then goes on to describesimplified models to illustrate aeroelastic behaviour and aircraftresponse and loads for the flexible aircraft before introducingsome more advanced methodologies. Finally, it explains howindustrial certification requirements for aeroelasticity and loadsmay be met and relates these to the earlier theoretical approachesused. Key features of this new edition include: -Uses a unified simple aeroelastic model throughout thebook -Major revisions to chapters on aeroelasticity -Updates and reorganisation of chapters involving FiniteElements -Some reorganisation of loads material -Updates on certification requirements -Accompanied by a website containing a solutions manual, andMATLAB and SIMULINK programs that relate to the modelsused -For instructors who recommend this textbook, a series oflecture slides are also available Introduction to Aircraft aeroelasticity and Loads, SecondEdition is a must-have reference for researchers andpractitioners working in the aeroelasticity and loads fields, andis also an excellent textbook for senior undergraduate and graduatestudents in aerospace engineering."
  • "Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some more advanced methodologies. Finally, it explains how industrial certification requirement."@en
  • "Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements."@en
  • "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 th."@en

http://schema.org/genre

  • "Online-Publikation"
  • "Lehrbuch"
  • "Electronic books"
  • "Electronic books"@en
  • "Llibres electrònics"
  • "Livres électroniques"

http://schema.org/name

  • "飞机气动弹性力学及载荷导论"
  • "Introduction to Aircraft Aeroelasticity and Loads"@en
  • "Introduction to Aircraft Aeroelasticity and Loads"
  • "Fei ji qi dong dan xing li xue ji zai he dao lun"
  • "Fei ji qi dong tan xing li xue ji zai he dao lun = Introduction to aircraft aeroelasticity and loads"
  • "Introduction to aircraft aeroelasticity and dynamic loads"
  • "Introduction to aircraft aeroelasticity and dynamic loads"@en
  • "飛機氣動彈性力學及載荷導論 = Introduction to aircraft aeroelasticity and loads"
  • "Introduction to aircraft aeroelasticity and loads"
  • "Introduction to aircraft aeroelasticity and loads"@en
  • "飞机气动弹性力学及载荷导论 = Introduction to aircraft aeroelasticity and loads"