LEADER 04832nam  2200637 a 450 
001 9910815660103321
005 20230421050631.0
010   $a1-60086-246-2
010   $a1-60086-118-0
035   $a(CKB)2550000000072658
035   $a(EBL)3111549
035   $a(SSID)ssj0000566034
035   $a(PQKBManifestationID)12169300
035   $a(PQKBTitleCode)TC0000566034
035   $a(PQKBWorkID)10533784
035   $a(PQKB)10722473
035   $a(MiAaPQ)EBC3111549
035   $a(Au-PeEL)EBL3111549
035   $a(CaPaEBR)ebr10516653
035   $a(OCoLC)922978799
035   $a(EXLCZ)992550000000072658
100   $a19950515d1996      uy             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt
182   $cc
183   $acr
200 10$aStructural loads analysis for commercial transport aircraft$b[electronic resource] $etheory and practice /$fTed L. Lomax
210   $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc1996
215   $a1 online resource (297 p.)
225 1 $aAIAA education series
300   $aDescription based upon print version of record.
311   $a1-56347-114-0 
320   $aIncludes bibliographical references and index.
327   $a""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)""
327   $a""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""
327   $a""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""
327   $a""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""; ""6.3 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""
327   $a""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""
327   $a""8.6 Unsymmetrical Load Conditions""
410  0$aAIAA education series.
606   $aAirframes$xDesign and construction
606   $aStructural dynamics
606   $aTransport planes$xDesign and construction
615  0$aAirframes$xDesign and construction.
615  0$aStructural dynamics.
615  0$aTransport planes$xDesign and construction.
676   $a629.134/31
700   $aLomax$b Ted L$0501804
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910815660103321
996   $aStructural loads analysis for commercial transport aircraft$9727734
997   $aUNINA