Mechanical Vibrations in Spacecraft Design - J. Jaap Wijker

Mechanical Vibrations in Spacecraft Design

(Autor)

Buch | Hardcover
XVI, 436 Seiten
2003 | 2004
Springer Berlin (Verlag)
978-3-540-40530-6 (ISBN)
171,19 inkl. MwSt

All typical and special modal and response analysis methods, applied within the frame of the design of spacecraft structures, are described in this book. It therefore addresses graduate students and engineers in the aerospace field.

1 Introduction.- 2 Single Degree of Freedom System.- 3 Damping Models.- 4 Multi-Degrees of Freedom Linear Dynamic Systems.- 5 Modal Analysis.- 6 Natural Frequencies, an Approximation.- 7 Modal Effective Mass.- 8 Response Analysis.- 9 Transient-Response Analysis.- 10 Shock-Response Spectrum.- 11 Random Vibration of Linear Dynamic Systems.- 12 Low-Frequency Acoustic Loads, Structural Responses.- 13 Statistical Energy Analysis.- 14 Free-free Dynamic Systems, Inertia Relief.- 15 Mode Acceleration Method.- 16 Residual Vectors.- 17 Dynamic Model Reduction Methods.- 18 Component Mode Synthesis.- 19 Load Transformation Matrices.- References.- Author Index.

From the reviews:

"This book collects the most topics on mechanical vibration techniques applied in spacecraft design and in other areas of mechanical engineering. The contents of the book reflect the modern level of knowledge in the linear theory of vibrations. ... Because this book contains an extensive list of topics on mechanical vibration in aerospace field, it may be very useful to students, postgraduate students, engineers and scientists of the corresponding specializations." (Yuri N. Sankin, Zentralblatt MATH, Vol. 1059 (10), 2005)

Erscheint lt. Verlag 15.10.2003
Zusatzinfo XVI, 436 p.
Verlagsort Berlin
Sprache englisch
Maße 155 x 235 mm
Gewicht 806 g
Themenwelt Technik Luft- / Raumfahrttechnik
Schlagworte Component modal synthesis • Low frequency acoustic load and responses • Mechanical vibration • modal effective masses • Modal reduction • random vibration • Raumfahrt • shock response spectra • Vibration
ISBN-10 3-540-40530-5 / 3540405305
ISBN-13 978-3-540-40530-6 / 9783540405306
Zustand Neuware
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