Introduction to Aircraft Aeroelasticity and Loads.

Mostrar otras versiones (1)

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 v...

Descripción completa

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Wright, Jan R.
Otros Autores: Cooper, Jonathan E.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Hoboken : Wiley, 2014.
Edición:2nd ed.
Colección:Aerospace Series.
Temas:
Aeroelasticity.
Aéroélasticité.
Aeroelasticity
Acceso en línea:Texto completo

MARC

LEADER 00000cam a2200000Mu 4500
001 EBOOKCENTRAL_ocn898769287
003 OCoLC
005 20240329122006.0
006 m o d
007 cr |n|||||||||
008 141227s2014 xx o 000 0 eng d
040 |a EBLCP  |b eng  |e pn  |c EBLCP  |d OCLCQ  |d DEBSZ  |d OCLCQ  |d ZCU  |d MERUC  |d ICG  |d OCLCF  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d TKN  |d DKC  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL 
020 |a 9781118700426 
020 |a 1118700422 
029 1 |a AU@  |b 000058373695 
029 1 |a DEBBG  |b BV044072544 
029 1 |a DEBSZ  |b 431886822 
029 1 |a DEBSZ  |b 456577769 
035 |a (OCoLC)898769287 
050 4 |a TL672 .W384 2014 
082 0 4 |a 668.1092368 
049 |a UAMI 
100 1 |a Wright, Jan R. 
245 1 0 |a Introduction to Aircraft Aeroelasticity and Loads. 
250 |a 2nd ed. 
260 |a Hoboken :  |b Wiley,  |c 2014. 
300 |a 1 online resource (605 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Aerospace Series 
588 0 |a Print version record. 
505 0 |a Title Page; Copyright Page; Contents; Series Preface; Preface to the Second Edition; Preface to the First Edition; Abbreviations; Introduction; Part I Background Material; Chapter 1 Vibration of Single Degree of Freedom Systems; 1.1 Setting up Equations of Motion for SDoF Systems; 1.1.1 Example: Classical SDoF System; 1.1.2 Example: Aircraft Control Surface; 1.2 Free Vibration of SDoF Systems; 1.2.1 Example: Aircraft Control Surface; 1.3 Forced Vibration of SDoF Systems; 1.4 Harmonic Forced Vibration -- Frequency Response Functions; 1.4.1 Response to Harmonic Excitation. 
505 8 |a 1.4.2 Frequency Response Functions1.4.3 Hysteretic (or Structural) Damping; 1.5 Transient/Random Forced Vibration -- Time Domain Solution; 1.5.1 Analytical Approach; 1.5.2 Principle of Superposition; 1.5.3 Example: Single Cycle of Square Wave Excitation -- Response Determined by Superposition; 1.5.4 Convolution Approach; 1.5.5 Direct Solution of Ordinary Differential Equations; 1.5.6 Example: Single Cycle of Square Wave Excitation -- Response Determined by Numerical Integration; 1.6 Transient Forced Vibration -- Frequency Domain Solution; 1.6.1 Analytical Fourier Transform. 
505 8 |a 1.6.2 Frequency Domain Response -- Excitation Relationship1.6.3 Example: Single Cycle of Square Wave Excitation -- Response Determined via Fourier Transform; 1.7 Random Forced Vibration -- Frequency Domain Solution; 1.8 Examples; Chapter 2 Vibration of Multiple Degree of Freedom Systems; 2.1 Setting up Equations of Motion; 2.2 Undamped Free Vibration; 2.2.1 Direct Approach; 2.2.2 Eigenvalue Approach; 2.2.3 Example: `Chain-like ́ 2DoF System; 2.3 Damped Free Vibration; 2.3.1 Example: 2DoF `Chain-Like ́ System with Proportional Damping. 
505 8 |a 2.3.2 Example: 2DoF `Chain-Like ́ System with Non-proportional Damping2.4 Transformation to Modal Coordinates; 2.4.1 Modal Coordinates; 2.4.2 Example: 2DoF `Chain-like ́ System with Proportional Damping; 2.4.3 Example: 2DoF `Chain-like ́ System with Non-proportional Damping; 2.4.4 Mode Shape Normalization; 2.4.5 Meaning of Modal Coordinates; 2.4.6 Dimensions of Modal Coordinates; 2.4.6.1 Consistent Coordinates; 2.4.6.2 Mixed Coordinates; 2.4.7 Model Order Reduction; 2.5 Two-DoF Rigid Aircraft in Heave and Pitch; 2.6 `Free-Free ́ Systems; 2.7 Harmonic Forced Vibration. 
505 8 |a 2.7.1 Equations in Physical Coordinates2.7.2 Equations in Modal Coordinates; 2.8 Transient/Random Forced Vibration -- Time Domain Solution; 2.8.1 Analytical Approach; 2.8.2 Convolution Approach; 2.8.3 Solution of Ordinary Differential Equations; 2.9 Transient Forced Vibration -- Frequency Domain Solution; 2.10 Random Forced Vibration -- Frequency Domain Solution; 2.11 Examples; Chapter 3 Vibration of Continuous Systems -- Assumed Shapes Approach; 3.1 Continuous Systems; 3.2 Modelling Continuous Systems; 3.3 Elastic and Flexural Axes; 3.4 Rayleigh-Ritz `Assumed Shapes ́ Method. 
500 |a 3.4.1 One-dimensional Systems. 
520 |a 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. 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Aeroelasticity. 
650 6 |a Aéroélasticité. 
650 7 |a Aeroelasticity  |2 fast 
700 1 |a Cooper, Jonathan E. 
758 |i has work:  |a Introduction to aircraft aeroelasticity and loads (Text)  |1 https://id.oclc.org/worldcat/entity/E39PCGxghKRmGFcTTrDdHXCWjC  |4 https://id.oclc.org/worldcat/ontology/hasWork 
776 0 8 |i Print version:  |a Wright, Jan R.  |t Introduction to Aircraft Aeroelasticity and Loads.  |d Hoboken : Wiley, ©2014  |z 9781118488010 
830 0 |a Aerospace Series. 
856 4 0 |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=1901847  |z Texto completo 
938 |a EBL - Ebook Library  |b EBLB  |n EBL1901847 
994 |a 92  |b IZTAP 

Ejemplares similares