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Record Nr. |
UNINA9910815660103321 |
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Autore |
Lomax Ted L |
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Titolo |
Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax |
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Pubbl/distr/stampa |
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Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 |
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ISBN |
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1-60086-246-2 |
1-60086-118-0 |
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Descrizione fisica |
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1 online resource (297 p.) |
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Collana |
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Disciplina |
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Soggetti |
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Airframes - Design and construction |
Structural dynamics |
Transport planes - Design and construction |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Description based upon print version of record. |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Nomenclature""; ""Chapter 1. Introduction""; ""1.1 Applicability of the Analysis""; ""1.2 Criteria""; ""1.3 Methodogy""; ""1.4 Static Aeroelastic Phenomena""; ""1.5 Sign Convention""; ""Chapter 2. Symmetrical Maneuvering Flight""; ""2.1 Symmetrical Maneuvering Flight Definition""; ""2.2 Symmetrical Maneuver Load Factors""; ""2.3 Steady-State Symmetrical Maneuvers""; ""2.4 Abrupt Pitching Maneuvers""; ""2.5 Abrupt Unchecked Pitch Maneuvers""; ""2.6 Abrupt Checked Maneuvers (Commercial Requirements)"" |
""2.7 Abrupt Checked Maneuvers (Military Requirements)""""2.8 Minimum Pitch Acceleration Requirements""; ""Chapter 3. Rolling Maneuvers""; ""3.1 Parameters Required for Structural Load Analyses""; ""3.2 Symmetrical Load Factors for Rolling Maneuvers""; ""3.3 Control Surface Deflections for Rolling Maneuvers""; ""3.4 Equations of Motion for Rolling Maneuvers""; ""3.5 Maximum Rolling Acceleration and Velocity Criteria""; ""3.6 Roll Termination Condition""; ""3.7 Nonlinear Lateral Control Inputs""; ""3.8 Aeroelastic Effects""; ""Chapter 4. Yawing Maneuvers"" |
""4.1 Parameters Required for Structural Load Analyses""""4.2 Rudder Maneuver Requirements FAR 25 Criteria""; ""4.3 Engine-Out Maneuver |
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