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230930s2023 vau o ||| 0 eng d |
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|a EBLCP
|b eng
|c EBLCP
|d YDX
|d OCLCO
|d OCLCQ
|d OCLCL
|d UUM
|d OCLCO
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| 019 |
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|a 1399462389
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|a 9781624106170
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|a 162410617X
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|z 1624106161
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|z 9781624106163
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|a (OCoLC)1401057166
|z (OCoLC)1399462389
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|a TL570
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| 049 |
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|a HCDD
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| 100 |
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|a Schmidt, David K.
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| 245 |
1 |
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|a Modern Flight Dynamics
|h [electronic resource].
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| 260 |
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|a Reston, VA :
|b American Institute of Aeronautics & Astronautics,
|c 2023.
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| 300 |
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|a 1 online resource (974 p.).
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| 490 |
1 |
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|a AIAA Education Series
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| 500 |
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|a Description based upon print version of record.
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| 505 |
0 |
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|a Intro -- Title Page -- Copyright Page -- About the Author -- Contents -- Acknowledgements -- Preface -- Nomenclature -- Chapter 1: Introduction and Topical Review -- 1.1 Small Perturbation Theory for Nonlinear Systems -- 1.2 Coordinate Systems -- 1.3 Vectors, Coordinate Transformations, and Direction-Cosine Matrices -- 1.4 Vector Differentiation -- 1.5 Newton's Second Law -- 1.6 Small Perturbation Analysis Revisited -- 1.7 Summary -- 1.8 Problems -- References -- Chapter 2: Equations of Motion of the Rigid Vehicle -- 2.1 Vector Equations of Motion-Flat Earth
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| 505 |
8 |
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|a 2.2 Scalar Equations of Motion-Flat Earth -- 2.3 Reference and Perturbation Equations-Flat Earth -- 2.4 Effects of Rotating Masses -- 2.5 Effects of Variable Mass -- 2.6 Effects of a Spherical, Rotating Earth -- 2.7 Point-Mass Performance Equations -- 2.8 Summary -- 2.9 Problems -- References -- Chapter 3: Structural Vibrations-A "Just-In-Time Tutorial" -- 3.1 Lumped-Mass Idealizations and Lagrange's Equation -- 3.2 Modal Analysis -- 3.3 Orthogonality of the Vibration Modes -- 3.4 Rigid-Body Degrees of Freedom -- 3.5 Reference Axes and Relative Motion
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| 505 |
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|a 3.6 Modal Analysis of the Generalized Eigensolution -- 3.7 Multi-Directional Motion -- 3.8 Preferred Derivation of Equations of Motion -- 3.9 Forced Motion and Virtual Work -- 3.10 Forced Motion of the Unrestrained Beam Model -- 3.11 Summary -- 3.12 Problems -- References -- Chapter 4: Equations of Motion for Elastic Vehicles -- 4.1 Lagrange's Equation-Kinetic and Potential Energies -- 4.2 The Vehicle-Fixed Frame-The Mean Axes -- 4.3 Modal Expansion Using Free-Vibration Modes -- 4.4 Selection of the Generalized Coordinates -- 4.5 Equations of Motion Governing Rigid-Body Translation
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| 505 |
8 |
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|a 4.6 Equations of Motion Governing Rigid-Body Rotation -- 4.7 Equations of Motion Governing Elastic Deformation -- 4.8 Motion of a particular point on the Elastic Vehicle -- 4.9 Reference and Perturbation Equation Sets for Perturbation Analysis -- 4.10 Summary -- 4.11 Problems -- References -- Chapter 5: Basic Aerodynamics of Lifting Surfaces -- 5.1 Subsonic Airfoil Section Characteristics -- 5.2 Effects of Flaps on Subsonic Airfoil Section Characteristics -- 5.3 Wing Planform Characteristics -- 5.4 Effects of Flaps on Wing Aerodynamic Characteristics -- 5.5 Downwash -- 5.6 Summary -- 5.7 Problems
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| 504 |
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|a References -- Chapter 6: Modeling the Forces and Moments on the Vehicle -- 6.1 Taylor-Series Expansion of Aerodynamic Forces and Moments -- 6.2 Aerodynamic Forces and Moments Acting on the Vehicle -- 6.3 Propulsive Forces and Moments Acting on the Vehicle -- 6.4 Fuselage-Reference and Stability Axes -- 6.5 Aerodynamic and Propulsive Forces and Moments at the Reference Condition -- 6.6 Forces and Moments due to Translational Velocity Perturbations -- 6.7 Forces and Moments due to Angular-Velocity Perturbations -- 6.8 E ffects of Atmospheric Turbulence on the Forces and Moments
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| 500 |
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|a 6.9 Dimensional Versus Nondimensional Derivatives
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| 520 |
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|a When introduced to the topic of aircraft flight dynamics students discover that it is the essence of aeronautical engineering because it involves the study of the motion--the flight--of the vehicle. This motion defines the vehicle's performance, a topic of enormous significance to the ultimate success of the machine. Flight dynamics is a study of the complete vehicle, rather than just a component of a vehicle. Hence, it is fundamentally the study of a multicom.
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| 650 |
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|a Aerodynamics.
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| 650 |
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|a Flight engineering.
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| 650 |
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0 |
|a Flight control.
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| 650 |
|
7 |
|a aerodynamics.
|2 aat
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| 758 |
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|i has work:
|a Modern flight dynamics (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGGcWfWjGWhkMBxVtvQVVK
|4 https://id.oclc.org/worldcat/ontology/hasWork
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| 776 |
0 |
8 |
|i Print version:
|a Schmidt, David K.
|t Modern Flight Dynamics
|d Reston, VA : American Institute of Aeronautics & Astronautics,c2023
|z 9781624106163
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| 830 |
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0 |
|a AIAA education series.
|
| 856 |
4 |
0 |
|u https://ebookcentral.proquest.com/lib/holycrosscollege-ebooks/detail.action?docID=30751532
|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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