000 | 07695nam a22005053i 4500 | ||
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001 | EBC3111549 | ||
003 | MiAaPQ | ||
005 | 20240729124521.0 | ||
006 | m o d | | ||
007 | cr cnu|||||||| | ||
008 | 240724s1995 xx o ||||0 eng d | ||
020 |
_a9781600861185 _q(electronic bk.) |
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020 | _z9781563471148 | ||
035 | _a(MiAaPQ)EBC3111549 | ||
035 | _a(Au-PeEL)EBL3111549 | ||
035 | _a(CaPaEBR)ebr10516653 | ||
035 | _a(OCoLC)922978799 | ||
040 |
_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ |
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050 | 4 | _aTL671.6 -- .L597 1996eb | |
082 | 0 | _a629.134/31 | |
100 | 1 | _aLomax, Ted L. | |
245 | 1 | 0 |
_aStructural Loads Analysis : _bTheory and Practice for Commercial Aircraft. |
250 | _a1st ed. | ||
264 | 1 |
_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c1995. |
|
264 | 4 | _c©1996. | |
300 | _a1 online resource (297 pages) | ||
336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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490 | 1 | _aAIAA Education Series | |
505 | 0 | _aCover -- 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 Requirements - FAR 25 Criteria -- 4.4 Equations of Motion for Yawing Maneuvers -- Chapter 5. Flight in Turbulence -- 5.1 Sharp-Edge Gust Criteria Based on Wing Loading -- 5.2 Revised Gust Criteria Using Airplane Mass Ratio -- 5.3 FAR/JAR Discrete Gust Design Criteria -- 5.4 Continuous Turbulence Gust Loads Criteria -- 5.5 Vertical Discrete Gust Considerations -- 5.6 Transient Lift Functions -- 5.7 Vertical Gust Continuous Turbulence Considerations -- 5.8 Multiple DOF Analyses -- 5.9 Lateral Gust Considerations -- 5.10 Oblique Gusts -- 5.11 Head-On Gusts -- Chapter 6. Landing Loads -- 6.1 Criteria per FAR/JAR 25.473 -- 6.2 Landing Speed Calculations. | |
505 | 8 | _a6.3 Two-Point Landing Conditions -- 6.4 Three-Point Landing Conditions -- 6.5 One-Gear Landing Conditions -- 6.6 Side Load Conditions -- 6.7 Rebound Landing Conditions -- 6.8 Landing Gear Shock Absorption and Drop Tests -- 6.9 Elastic Airplane Analysis -- 6.10 Automatic Ground Spoilers -- Chapter 7. Ground-Handling Loads -- 7.1 Ground-Handling Conditions -- 7.2 Static Load Conditions -- 7.3 Taxi, Takeoff, and Landing Roll Conditions -- 7.4 Braked-Roll Conditions -- 7.5 Refused Takeoff Considerations -- 7.6 Turning Conditions -- 7.7 Towing Conditions -- 7.8 Jacking Loads per FAR/JAR 25.519 -- 7.9 Tethering Problem -- Chapter 8. Horizontal Tail Loads -- 8.1 Horizontal Tail Design Load Envelopes -- 8.2 Balanced Maneuver Analysis -- 8.3 Abrupt Unchecked Elevator Conditions -- 8.4 Checked Maneuver Conditions -- 8.5 Vertical Gust Conditions -- 8.6 Unsymmetrical Load Conditions -- 8.7 Stall Buffet Considerations -- 8.8 High-Speed Buffet Considerations -- Chapter 9. Vertical Tail Loads -- 9.1 Vertical Tail Loads for Yawing Maneuvers -- 9.2 Vertical Tail Loads for Rudder Maneuver Conditions -- 9.3 Vertical Tail Loads Engine-Out Conditions -- 9.4 Vertical Tail Loads Using the Gust Formula Approach -- 9.5 Lateral Gust Dynamic Analyses -- 9.6 Definition of Vertical Tail for Structural Analysis -- 9.7 Lateral Bending-Body Flexibility Parameters -- 9.8 Relationship Between Sideslip Angle and Fin Angle of Attack -- Chapter 10. Wing Loads -- 10.1 Wing Design Criteria -- 10.2 Wing Design Conditions -- 10.3 Symmetrical Maneuver Analysis -- 10.4 Rolling Maneuver Analysis -- 10.5 Yawing Conditions -- 10.6 Landing and Ground-Handling Static Load Conditions -- 10.7 Gust Loads and Consideration for Dynamics -- 10.8 Wing Loads for Dynamic Landing Analysis -- 10.9 Wing Loads for Dynamic Taxi Analysis -- 10.10 Effect of Speedbrakes on Symmetrical Flight Conditions. | |
505 | 8 | _a10.11 Effect of Fuel Usage on Wing Loads -- 10.12 Wing Loads for Structural Analysis -- 10.13 Simplified Shear Flow Calculations for Spars -- 10.14 Wing Spanwise Load Distributions -- Chapter 11. Body Monocoque Loads -- 11.1 Monocoque Analysis Criteria -- 11.2 Monocoque Design Conditions -- 11.3 Load Factors Acting on the Body -- 11.4 Pay load Distribution for Monocoque Analysis -- 11.5 Monocoque Payload Limitations -- 11.6 Cabin Pressure Criteria -- Chapter 12. Control Surface Loads and High-Lift Devices -- 12.1 Control Surface Loads -- 12.2 Determination of Maximum Available Control Surface Angle -- 12.3 Control Surface Airload Distribution -- 12.4 Tab Design Airload -- 12.5 Spoiler Load Distribution -- 12.6 Structural Deformation of Control Surface Hinge Lines -- 12.7 High- Lift Devices -- Chapter 13. Static Aeroelastic Considerations -- 13.1 Flutter, Deformation, and Fail-Safe Criteria -- 13.2 Static Divergence Analysis -- 13.3 Control Surface Reversal Analysis -- 13.4 Structural Stiffness Considerations -- Chapter 14. Structural Design Considerations -- 14.1 Gross Weights -- 14.2 Center of Gravity Limits -- 14.3 Selection of Positive and Negative C[sub(Lmax)] -- 14.4 V-n Diagrams -- 14.5 Maneuvering Envelope -- 14.6 Gust Envelope -- Chapter 15. Structural Design Airspeeds -- 15.1 Cruise and Dive Speeds -- 15.2 Maneuvering Speeds -- 15.3 Flap Placard Speeds and Altitude Limitations -- 15.4 Gust Design Speeds -- 15.5 Turbulent Air Penetration Speeds V[sub(RA)] -- 15.6 Landing Gear Placards -- 15.7 Bird Strike Airspeed Considerations -- 15.8 Stall Speeds -- Chapter 16. Airspeeds for Structural Engineers -- 16.1 Relationship of Lift to Airspeed -- 16.2 Equivalent Airspeed -- 16.3 Relationship Between Equivalent Airspeed and True Airspeed -- 16.4 Indicated Airspeed -- 16.5 Calibrated Airspeed -- 16.6 True Airspeed. | |
505 | 8 | _a16.7 Variation of Equivalent Airspeed and True Airspeed with Altitude -- Subject Index -- A -- B -- C -- D -- E -- F -- G -- H -- I -- J -- K -- L -- M -- N -- O -- P -- R -- S -- T -- U -- V -- W -- Y -- Z. | |
588 | _aDescription based on publisher supplied metadata and other sources. | ||
590 | _aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries. | ||
650 | 0 | _aAirframes -- Design and construction. | |
650 | 0 | _aStructural dynamics. | |
650 | 0 | _aTransport planes -- Design and construction. | |
655 | 4 | _aElectronic books. | |
776 | 0 | 8 |
_iPrint version: _aLomax, Ted L. _tStructural Loads Analysis _dReston : American Institute of Aeronautics and Astronautics,c1995 _z9781563471148 |
797 | 2 | _aProQuest (Firm) | |
830 | 0 | _aAIAA Education Series | |
856 | 4 | 0 |
_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111549 _zClick to View |
999 |
_c68216 _d68216 |