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Introduction to Aircraft Aeroelasticity & Load

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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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Ketersediaan

Informasi Detail

Judul Seri

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No. Panggil

629.132 JAN i

Penerbit

Chichester, England : John Wiley & Sons, Ltd., 2015

Deskripsi Fisik

xxiv, 499 pages : illustrations.

Bahasa

English

ISBN/ISSN

9781118488010

Klasifikasi

629.132 JAN i

Tipe Isi

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Tipe Media

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Tipe Pembawa

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Edisi

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Subjek

TRANSPORTATION
Aeroelasticity

Info Detail Spesifik

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Pernyataan Tanggungjawab

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Versi lain/terkait

Lampiran Berkas

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