Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity (Record no. 60633)
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| fixed length control field | 05524nam a22006015i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-031-50054-1 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | DE-He213 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20251030112305.0 |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION | |
| fixed length control field | cr nn 008mamaa |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240611s2024 sz | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9783031500541 |
| -- | 978-3-031-50054-1 |
| 024 7# - OTHER STANDARD IDENTIFIER | |
| Standard number or code | 10.1007/978-3-031-50054-1 |
| Source of number or code | doi |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER | |
| Classification number | TL1-4050 |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TRP |
| Source | bicssc |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TTDS |
| Source | bicssc |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TEC002000 |
| Source | bisacsh |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TRP |
| Source | thema |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TTDS |
| Source | thema |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Demasi, Luciano. |
| Relator term | author. |
| Relator code | aut |
| -- | http://id.loc.gov/vocabulary/relators/aut |
| 9 (RLIN) | 78503 |
| 245 10 - TITLE STATEMENT | |
| Title | Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity |
| Medium | [electronic resource] / |
| Statement of responsibility, etc. | by Luciano Demasi. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. 2024. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Cham : |
| Name of producer, publisher, distributor, manufacturer | Springer Nature Switzerland : |
| -- | Imprint: Springer, |
| Date of production, publication, distribution, manufacture, or copyright notice | 2024. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | XXIII, 831 p. 232 illus., 230 illus. in color. |
| Other physical details | online resource. |
| 336 ## - CONTENT TYPE | |
| Content type term | text |
| Content type code | txt |
| Source | rdacontent |
| 337 ## - MEDIA TYPE | |
| Media type term | computer |
| Media type code | c |
| Source | rdamedia |
| 338 ## - CARRIER TYPE | |
| Carrier type term | online resource |
| Carrier type code | cr |
| Source | rdacarrier |
| 347 ## - DIGITAL FILE CHARACTERISTICS | |
| File type | text file |
| Encoding format | |
| Source | rda |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Finite-Part Integrals -- Convolution and Duhamel Integrals -- Laplace and Fourier Transforms -- Review of the Least Square Method -- Vector Identities Used in Aerodynamics -- Reynolds Transport Theorem, Isentropic, Continuity, and Momentum Equations -- Vorticity, and Kelvin’s Circulation Theorem -- Velocity Potential -- The Biot Savart Law for Incompressible Fluids -- The Fluid-Structure Boundary Condition -- The Aerodynamic Force for the Steady Incompressible Ideal Flow -- Small Perturbation Theory -- Small Perturbation Acceleration Potential -- Compressible Fluid at Rest -- Compressible Fluid in Motion -- Compressible Fluid in Motion: the Doublet Solution -- Theoretical Aerodynamic Modeling of Wings -- Steady Incompressible Ideal Flow and Modeling of Finite Wings -- Two-Dimensional Unsteady Incompressible Flow -- Harmonic Motion, Reduced Frequency, and Kernel -- The Generalized Aerodynamic Force for the Continuous System -- Finite-Element Time Domain Aeroelastic Equations -- Laplace and Fourier Transformed Discrete Aeroelastic Equations -- The Unsteady Kernel -- Industry Standard Doublet Lattice Implementation -- Structural Dynamics: the Concept of Free Vibration Modes -- From the Structural Mesh to the Aerodynamic Mesh: Splining -- Generalized Aerodynamic Force Matrix and Rational Function Approximation -- Equations of Motion in the Laplace Domain with the Use of Rational Function Approximation -- Stability Analysis in the Laplace Domain -- Linear Time-Invariant Systems and Stability -- Linear Time-Invariant Aeroelastic Systems -- Classical Flutter, State Space Model, and Root Locus -- Introduction to the Concept of Body Freedom Flutter -- An Introduction to Nonlinear Aeroelasticity -- An Introduction to Nonlinear Dynamics. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | Aeroelasticity is an essential discipline for the design of airplanes, unmanned systems, and innovative configurations. This book introduces the subject of unsteady aerodynamics and dynamic aeroelasticity by presenting industry-standard techniques, such as the Doublet Lattice Method for nonplanar wing systems. “Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity'' is a useful reference for aerospace engineers and users of NASTRAN and ZAERO but is also an excellent complementary textbook for senior undergraduate and graduate students. Fully develops the theory of acceleration potential, fundamental to the unsteady aerodynamics behind the Doublet Lattice Method; Explains fully the industry-standard unsteady aerodynamics capability: the Doublet Lattice Method; Theoretically develops various state-of-the-art methods to determine the flutter point; Clarifies the differences between ``cantilever flutter’’ and ``body freedom flutter’’; Introduces the nonlinear aeroelasticity of Joined Wings and innovative wing systems. Luciano Demasi has written a comprehensive and insightful book on aeroelasticity as practiced today. The careful and deep attention to the fundamentals and a unique and valuable discussion of the implementation of Doublet Lattice aerodynamics are special features of the book. The author also ranges over a number of additional topics including current and promising aircraft and wing concepts that bring new challenges to the aeroelastician. The student new to the topic as well as the experienced practitioner will find much to ponder and benefit from a careful reading of this text. — Prof. Earl Dowell, Duke University. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 9 (RLIN) | 66335 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 9 (RLIN) | 66336 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | |
| 9 (RLIN) | 66337 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | |
| 9 (RLIN) | 66339 |
| 650 24 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | |
| 9 (RLIN) | 66340 |
| 650 24 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 650 24 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 650 24 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
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| 9 (RLIN) | 65620 |
| 710 2# - ADDED ENTRY--CORPORATE NAME | |
| Corporate name or jurisdiction name as entry element | SpringerLink (Online service) |
| 773 0# - HOST ITEM ENTRY | |
| Title | Springer Nature eBook |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Printed edition: |
| International Standard Book Number | 9783031500534 |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Printed edition: |
| International Standard Book Number | 9783031500558 |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Printed edition: |
| International Standard Book Number | 9783031500565 |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://doi.org/10.1007/978-3-031-50054-1">https://doi.org/10.1007/978-3-031-50054-1</a> |
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