Introduction to Structural Dynamics and Aeroelasticity by Dewey H Hodges

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eBay item number:394185223924
Last updated on Dec 09, 2025 13:00:03 PSTView all revisionsView all revisions

Item specifics

Condition
Good: A book that has been read but is in good condition. Very minimal damage to the cover including ...
Publish Year
2002
Updated ISBN1
110761709X
Updated ISBN2
9781107617094
ISBN
9780521806985
Subject Area
Technology & Engineering
Publication Name
Introduction to Structural Dynamics and Aeroelasticity
Publisher
Cambridge University Press
Item Length
10.4 in
Subject
Engineering (General), Structural, Aeronautics & Astronautics
Publication Year
2002
Series
Cambridge Aerospace Ser.
Type
Textbook
Format
Hardcover
Language
English
Item Height
0.7 in
Author
G. Alvin Pierce, Dewey H. Hodges
Item Weight
17.8 Oz
Item Width
7.2 in
Number of Pages
184 Pages
Category

About this product

Product Identifiers

Publisher
Cambridge University Press
ISBN-10
0521806984
ISBN-13
9780521806985
eBay Product ID (ePID)
1940191

Product Key Features

Number of Pages
184 Pages
Publication Name
Introduction to Structural Dynamics and Aeroelasticity
Language
English
Subject
Engineering (General), Structural, Aeronautics & Astronautics
Publication Year
2002
Type
Textbook
Subject Area
Technology & Engineering
Author
G. Alvin Pierce, Dewey H. Hodges
Series
Cambridge Aerospace Ser.
Format
Hardcover

Dimensions

Item Height
0.7 in
Item Weight
17.8 Oz
Item Length
10.4 in
Item Width
7.2 in

Additional Product Features

Intended Audience
Scholarly & Professional
LCCN
2001-052552
Reviews
"Wonderfully written and full of vital information by two unequalled experts on the subject, this text meets the need for an up-to-date treatment of structural dynamics and aeroelasticity for advanced undergraduate or beginning graduate aerospace engineering students." Current Engineering Practice, "...a welcome addition to the textbooks available to those with interest in aeroelasticity.... As a textbook, it serves as an excellent resource for advanced undergraduate and entry-level graduate courses in aeroelasticity.... Furthermore, practicing engineers interested in a background in aeroelasticity will find the text to be a friendly primer." AIAA Bulletin, "Hodges and Pierce have written this significant publication to fill an important gap in aeronautical engineering education. Highly recommended." Choice
Dewey Edition
21
Series Volume Number
Series Number 15
Illustrated
Yes
Dewey Decimal
629.134/31
Table Of Content
1. Introduction; 2. Structural dynamics; 3. Static aeroelasticity; 4. Aeroelastic flutter; Bibliography; Appendix A: Lagrange's equation; Index.
Synopsis
Here is an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity and dynamic aeroelasticity. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. Over one hundred illustrations and tables help clarify the text, while more than fifty problems enhance student learning., This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning., Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.
LC Classification Number
TL671.6 .H565 2002

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