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ocn774285679 |
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OCoLC |
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20240623213015.0 |
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990111s1999 vaua ob 001 0 eng d |
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|a (OCoLC)774285679
|z (OCoLC)872076321
|z (OCoLC)922978645
|z (OCoLC)961671045
|z (OCoLC)962608750
|z (OCoLC)988436624
|z (OCoLC)991917285
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4 |
|a TL671.6
|b .B57 1999eb
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| 049 |
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|a HCDD
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| 100 |
1 |
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|a Bismarck-Nasr, Maher N.,
|d 1940-
|1 https://id.oclc.org/worldcat/entity/E39PCjKWgcvvbRxYkX7j8kMfpX
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| 245 |
1 |
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|a Structural dynamics in aeronautical engineering /
|c Maher N. Bismarck-Nasr.
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| 260 |
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|a Reston, Va. :
|b American Institute of Aeronautics and Astronautics, Inc.,
|c ©1999.
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| 300 |
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|a 1 online resource (xiv, 293 pages) :
|b illustrations
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
1 |
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|a AIAA education series
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| 504 |
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|a Includes bibliographical references and index.
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| 520 |
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|a Annotation "Structural Dynamics in Aeronautical Engineering is a comprehensive introduction to the modern methods of dynamic analysis of aeronautical structures. The text represents carefully developed course materials, beginning with an introductory chapter on matrix algebra and methods for numerical computations, followed by a series of chapters discussing specific aeronautical applications. In this way, the student can be guided from the simple concept of a single-degree-of-freedom structural system to the more complex multidegree-of-freedom and continuous systems, including random vibrations, nonlinear systems, and aeroelastic phenomena. Among the various examples used in the text, the chapter on aeroelasticity of flight vehicles is particularly noteworthy with its clear presentation of the phenomena and its mathematical formulation for structural and aerodynamic loads.
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|a Cover -- Title -- Copyright -- Table of Contents -- Preface -- Chapter 1. Matrix Algebra and Techniques -- 1.1 Notations and Definitions -- 1.2 Matrix Algebra -- 1.3 Differentiation and Integration of Matrices -- 1.4 Transformations -- 1.5 Solution of Large Systems of Linear Equations -- 1.6 The Eigenvalue Problem -- References -- Problems -- Chapter 2. Single-Degree-of-Freedom Linear Systems -- 2.1 Equation of Motion -- 2.2 Free Vibration -- 2.3 Response to Harmonic Excitation -- 2.4 Response to an Impulsive Excitation
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|a 2.5 Response to a Step Excitation2.6 Response to Periodic Excitation (Fourier Series) -- 2.7 Response to Aperiodic Excitation (Fourier Transform) -- 2.8 Laplace Transform (Transfer Function) -- Problems -- Chapter 3. Multidegree-of-Freedom Linear Systems -- 3.1 Equations of Motion -- 3.2 Free Vibration: The Eigenvalue Problem -- 3.3 Response to an External Applied Load -- 3.4 Damping Effect -- 3.5 Applications -- References -- Problems -- Chapter 4. Dynamics of Continuous Elastic Bodies -- 4.1 Introduction -- 4.2 Slender Beams -- 4.3 Flat Plates
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|a 4.4 Shell Structures4.5 Response to Initial Conditions -- 4.6 Response to External Excitations -- References -- Problems -- Chapter 5. Nonlinear Systems -- 5.1 Introduction -- 5.2 Simple Examples of Nonlinear Systems -- 5.3 Physical Properties of Nonlinear Systems -- 5.4 Solutions of the Equation of Motion of a Single-Degree-of-Freedom Nonlinear System -- 5.5 Multidegree-of-Freedom Nonlinear Systems -- References -- Problems -- Chapter 6. Random Vibrations -- 6.1 Introduction -- 6.2 Classification of Random Processes
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| 505 |
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|a 6.3 Probability Distribution and Density Functions6.4 Description of the Mean Values in Terms of the Probability Density Function -- 6.5 Properties of the Autocorrelation Function -- 6.6 Power Spectral Density Function -- 6.7 Properties of the Power Spectral Density Function -- 6.8 White Noise and Narrow and Large Bandwidth -- 6.9 Single-Degree-of-Freedom Response -- 6.10 Response to a White Noise -- 6.11 Multidegree-of-Freedom Systems -- References -- Problems -- Chapter 7. The Typical Section in Aeroelasticity -- 7.1 Single-Degree-of-Freedom Stability
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| 505 |
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|a 7.2 The Typical Section7.3 Typical Section Using Unsteady Linearized Potential Theory -- 7.4 Typical Section with Control Surface -- 7.5 Control Surface Reversal and Efficiency -- References -- Problems -- Chapter 8. Aeroelasticity of Flight Vehicles -- 8.1 Introduction -- 8.2 Problem Formulation -- 8.3 Incremental Nonstationary Aerodynamic Loads -- 8.4 Modal Transformation -- 8.5 Solution of the Aeroelastic Stability Equations -- 8.6 Applications -- 8.7 Optimization to Satisfy Flutter Requirements -- References
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| 650 |
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|a Airframes
|x Mathematical models.
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| 650 |
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|a Space vehicles
|x Mathematical models.
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| 650 |
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|a Structural engineering
|x Mathematics.
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| 650 |
|
7 |
|a Airframes
|x Mathematical models
|2 fast
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| 650 |
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7 |
|a Space vehicles
|x Mathematical models
|2 fast
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| 650 |
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7 |
|a Structural engineering
|x Mathematics
|2 fast
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| 655 |
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7 |
|a dissertations.
|2 aat
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| 655 |
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|a Academic theses
|2 fast
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| 655 |
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|a Academic theses.
|2 lcgft
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| 655 |
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|a Thèses et écrits académiques.
|2 rvmgf
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| 758 |
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|i has work:
|a Structural dynamics in aeronautical engineering (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGHkFpbkpXhdF6bD6fXQtq
|4 https://id.oclc.org/worldcat/ontology/hasWork
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| 776 |
0 |
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|i Print version:
|a Bismarck-Nasr, Maher N., 1940-
|t Structural dynamics in aeronautical engineering.
|d Reston, Va. : American Institute of Aeronautics and Astronautics, Inc., ©1999
|w (DLC) 99012326
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| 830 |
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0 |
|a AIAA education series.
|
| 856 |
4 |
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|u https://ebookcentral.proquest.com/lib/holycrosscollege-ebooks/detail.action?docID=3111527
|y Click for online access
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| 903 |
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|a EBC-AC
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| 994 |
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|a 92
|b HCD
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