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Introduction to Aircraft Aeroelasticity & Load

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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Informasi Detail
Judul Seri
-
No. Panggil
629.132 JAN i
Penerbit
Chichester, England : John Wiley & Sons, Ltd.,
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
-
Edisi
-
Subjek
TRANSPORTATION
Aeroelasticity
Info Detail Spesifik
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Pernyataan Tanggungjawab
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