Introduction to Aircraft Aeroelasticity And Dynamic Loads - Couverture souple
Livre 74 sur 125: AIAA Education
Synopsis
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.
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Quatrième de couverture
Aircraft performance is influenced significantly both byaeroelastic phenomena, arising from the interaction of elastic,inertial and aerodynamic forces, and by load variations resultingfrom flight and ground manoeuvres and gust / turbulence encounters.There is a strong link between aeroelasticity and loads, and thesetopics have become increasingly integrated in recent years.
Introduction to Aircraft Aeroelasticity and Loads introduces thereader to the main principles involved in a wide range ofaeroelasticity and loads topics. Divided into three sections, thebook begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control. It goes on to describe simplifiedmodels to illustrate aeroelastic behaviour and aircraft responsebefore introducing more advanced methodologies. Finally, itexplains how industrial certification requirements foraeroelasticity and loads may be met and relates these to theearlier theoretical approaches used.
- Presents fundamentals of structural dynamics, aerodynamics,static and dynamic aeroelasticity, response and load calculationsand testing techniques.
- Covers performance issues related to aeroelasticity such asflutter, control effectiveness, divergence and redistribution oflift.
- Includes up–to–date experimental methods and analysis.
- Accompanied by a website with MatLAB and SIMULINK programs thatrelate to the models used.
- Introduction to Aircraft Aeroelasticity and Loads enables thereader to understand the aeroelastic and loads principles andprocedures employed in a modern aircraft design office. It willappeal to final year undergraduate and masters students as well asengineers who are new to the aerospace industry.
Présentation de l'éditeur
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