Airframe structural design : practical design information and data on aircraft structures / by Michael Chun-yung Niu
| Airframe structural design : practical design information and data on aircraft structures / by Michael Chun-yung Niu |
| Autore | Niu, Michael Chun-Yung |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Hong Kong : Conmilit Press, , 1999 |
| Descrizione fisica | 612 p. : ill. ; 29 cm |
| Disciplina | 629.13431 |
| Collana | Michael C.Y. Niu's airframe book series |
| Soggetto topico | Airframes - Design and construction |
| ISBN | 9627128090 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001021779707536 |
Niu, Michael Chun-Yung
|
||
| Hong Kong : Conmilit Press, , 1999 | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Assessment of industry practices for aircraft bonded joints and structures [[electronic resource] ] : final report
| Assessment of industry practices for aircraft bonded joints and structures [[electronic resource] ] : final report |
| Pubbl/distr/stampa | Washington, D.C. : , : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, , [2005] |
| Descrizione fisica | 1 volume : digital, PDF file |
| Soggetto topico |
Airframes - Design and construction
Adhesive joints |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Assessment of industry practices for aircraft bonded joints and structures |
| Record Nr. | UNINA-9910694697903321 |
| Washington, D.C. : , : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, , [2005] | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Bonded Joints and Repairs to Composite Airframe Structures [[electronic resource]]
| Bonded Joints and Repairs to Composite Airframe Structures [[electronic resource]] |
| Autore | Wang Chun Hui |
| Pubbl/distr/stampa | Saint Louis, : Elsevier Science, 2015 |
| Descrizione fisica | 1 online resource (0 p.) |
| Disciplina | 620.118 |
| Altri autori (Persone) | DuongCong N |
| Soggetto topico |
Fibrous composites
Airframes - Design and construction |
| ISBN |
0-12-417172-9
0-12-417153-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Preface ; Part 1. Analysis and design. Chapter 1. Introduction and overview ; 1.1. Aim of book ; 1.2. Criticality of structure and damage ; 1.3. Types of composite repairs and certification criteria ; 1.4. Overview of repair design and analysis process ; 1.5. Effect of load attraction in patch design ; 1.6. Effect of taper and scarf ratios on joint design ; 1.6.1. Safe-life approach ; 1.6.2. Damage tolerance approach ; 1.6.3. Stepped repairs ; 1.7. Summary ; References ; Chapter 2. Failure criteria ; 2.1. Introduction ; 2.2. Adhesive failure criteria ; 2.2.1. Failure criteria for brittle adhesives ; 2.2.2. Failure criteria for ductile adhesives ; 2.3. Composite failure criteria ; 2.3.1. Intralamina failure criteria ; 2.3.2. Interlaminar failure criteria ; 2.4. Summary ; References ; Chapter 3. Doubler joint analysis ; 3.1. Introduction ; 3.2. Untapered doublers and joints ; 3.2.1. Two-sided doublers and double strap joints ; 3.2.2. Elastic solution for adhesive peel and shear ; 3.3.3. Elastic-plastic solution for adhesive peel and shear ; 3.3.4. Effect of adherent shear deformation ; 3.3.5. Numerical examples ; 3.4. Summary ; References ; Chapter 4. Design of scarf and doubler-scarf joints ; 4.1. Introduction ; 4.2. Scarf joint of homogeneous adherends ; 4.2.1. Constant-angle scarf ; 4.2.2. Optimum angle of scarf between dissimilar materials 4.3. Composite scarf joints ; 4.3.1. Identical adherends with constant-angle scarf ; 4.3.2. Elasto-plastic stress analysis of scarf joints ; 4.4. Experiments and validation ; 4.4.1. Room temperature dry condition ; 4.4.2. Hot wet condition ; Doubler-scarf joints ; Conclusions ; References ; Chapter 5. Disbond and damage tolerance analysis of doubler repairs ; 5.1. Introduction ; 5.2. Analytical methods for delamination analysis ; 5.2.1. VCCT by FE method ; 5.2.2. Crack tip element approach ; 5.2.3. Cohesive zone model ; 5.3. Analytical methods for disbond analysis ; 5.4. Fatigue damage accumulation model for predicting interlaminar failure and disbond ; 5.5. Summary ; References ; Chapter 6. Damage tolerance and fatigue durability of scarf joints ; 6.1. Introduction ; 6.2. Impact damage of scarf joints and repairs ; 6.3. Effects of disbond on joint strength ; 6.4. Design methods ; 6.4.1. Average stress ; 6.4.2. Linear elastic fracture mechanics ; 6.4.3. Virtual crack closure technique (VCCT) ; 6.4.4. Cohesive zone model (CZM) ; 6.5. Verifications ; 6.5.1. Finite element model (FEM) ; 6.5.2. Strength prediction of scarf joints ; 6.6. Fatigue disbond growth life ; 6.6.1. Method ; 6.6.2. Experimental validation ; 6.6.3. Comparison between analysis and experiments ; 6.7. Discussion ; 6.8. Summary ; References ; Chapter 7. Design and analysis of doubler repairs ; 7.1. Introduction ; 7.2. Repair analysis for elliptical damages ; 7.2.1. Elastic solution for an elliptical hole in an anisotropic plate ; 7.2.2. Elastic solution for an elliptical inhomogeneity in a 2D anisotropic plate ; 7.2.3. Two-stage analysis procedure for determining load attraction and stress concentration ; 7.2.4. Strength assessment for an after repair damaged skin laminate ; 7.2.5. Bond line analysis by bonded joint or bonded doubler methods ; 7.3. Repair analysis for crack-line damages ; 7.3.1. Wang and Rose's crack bridging model ; 7.3.2. Two-stage analysis procedure for crack patching ; 7.4. Patch design for an elliptical damage ; 7.4.1. Design criteria and guidelines ; 7.4.2. Patch design algorithm 7.5. Summary ; References ; Chapter 8. Design and optimization of scarf repairs ; 8.1. Introduction ; 8.2. Residual strength of scarfed laminates ; 8.2.1. Tension and compression loading ; 8.2.2. Predictive modeling ; 8.3. Shape optimization of scarf repairs ; 8.3.1. Assessment of existing shaping methods 8.3.2. Optimum solution ; 8.3.3. Case studies ; 8.4. Structural doublers ; References -- Part 2. Manufacturing and inspection. Chapter 9. Repair manufacturing processes ; 9.1. Introduction ; 9.2. Scarfing operation ; 9.3. Repair patch manufacturing ; 9.3.1. Soft patch ; 9.3.2. Molded patch ; 9.4. Surface treatment ; 9.5. Adhesive bonding ; 9.6. Repair of thick laminates ; References ; Chapter 10. Non-destructive evaluation of bond ; 10.1. Introduction ; 10.2. Detection of disbonds ; 10.3. Detection of weak adhesion bonds ; 10.4. Local bond proof testing ; 10.5. Satellite coupon proof test ; References ; Index. |
| Record Nr. | UNINA-9910797617203321 |
Wang Chun Hui
|
||
| Saint Louis, : Elsevier Science, 2015 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Bonded Joints and Repairs to Composite Airframe Structures
| Bonded Joints and Repairs to Composite Airframe Structures |
| Autore | Wang Chun Hui |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Saint Louis, : Elsevier Science, 2015 |
| Descrizione fisica | 1 online resource (0 p.) |
| Disciplina |
620.118
629.13431 |
| Altri autori (Persone) | DuongCong N |
| Soggetto topico |
Fibrous composites
Airframes - Design and construction |
| ISBN |
9780124171725
0124171729 9780124171534 0124171532 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Preface ; Part 1. Analysis and design. Chapter 1. Introduction and overview ; 1.1. Aim of book ; 1.2. Criticality of structure and damage ; 1.3. Types of composite repairs and certification criteria ; 1.4. Overview of repair design and analysis process ; 1.5. Effect of load attraction in patch design ; 1.6. Effect of taper and scarf ratios on joint design ; 1.6.1. Safe-life approach ; 1.6.2. Damage tolerance approach ; 1.6.3. Stepped repairs ; 1.7. Summary ; References ; Chapter 2. Failure criteria ; 2.1. Introduction ; 2.2. Adhesive failure criteria ; 2.2.1. Failure criteria for brittle adhesives ; 2.2.2. Failure criteria for ductile adhesives ; 2.3. Composite failure criteria ; 2.3.1. Intralamina failure criteria ; 2.3.2. Interlaminar failure criteria ; 2.4. Summary ; References ; Chapter 3. Doubler joint analysis ; 3.1. Introduction ; 3.2. Untapered doublers and joints ; 3.2.1. Two-sided doublers and double strap joints ; 3.2.2. Elastic solution for adhesive peel and shear ; 3.3.3. Elastic-plastic solution for adhesive peel and shear ; 3.3.4. Effect of adherent shear deformation ; 3.3.5. Numerical examples ; 3.4. Summary ; References ; Chapter 4. Design of scarf and doubler-scarf joints ; 4.1. Introduction ; 4.2. Scarf joint of homogeneous adherends ; 4.2.1. Constant-angle scarf ; 4.2.2. Optimum angle of scarf between dissimilar materials 4.3. Composite scarf joints ; 4.3.1. Identical adherends with constant-angle scarf ; 4.3.2. Elasto-plastic stress analysis of scarf joints ; 4.4. Experiments and validation ; 4.4.1. Room temperature dry condition ; 4.4.2. Hot wet condition ; Doubler-scarf joints ; Conclusions ; References ; Chapter 5. Disbond and damage tolerance analysis of doubler repairs ; 5.1. Introduction ; 5.2. Analytical methods for delamination analysis ; 5.2.1. VCCT by FE method ; 5.2.2. Crack tip element approach ; 5.2.3. Cohesive zone model ; 5.3. Analytical methods for disbond analysis ; 5.4. Fatigue damage accumulation model for predicting interlaminar failure and disbond ; 5.5. Summary ; References ; Chapter 6. Damage tolerance and fatigue durability of scarf joints ; 6.1. Introduction ; 6.2. Impact damage of scarf joints and repairs ; 6.3. Effects of disbond on joint strength ; 6.4. Design methods ; 6.4.1. Average stress ; 6.4.2. Linear elastic fracture mechanics ; 6.4.3. Virtual crack closure technique (VCCT) ; 6.4.4. Cohesive zone model (CZM) ; 6.5. Verifications ; 6.5.1. Finite element model (FEM) ; 6.5.2. Strength prediction of scarf joints ; 6.6. Fatigue disbond growth life ; 6.6.1. Method ; 6.6.2. Experimental validation ; 6.6.3. Comparison between analysis and experiments ; 6.7. Discussion ; 6.8. Summary ; References ; Chapter 7. Design and analysis of doubler repairs ; 7.1. Introduction ; 7.2. Repair analysis for elliptical damages ; 7.2.1. Elastic solution for an elliptical hole in an anisotropic plate ; 7.2.2. Elastic solution for an elliptical inhomogeneity in a 2D anisotropic plate ; 7.2.3. Two-stage analysis procedure for determining load attraction and stress concentration ; 7.2.4. Strength assessment for an after repair damaged skin laminate ; 7.2.5. Bond line analysis by bonded joint or bonded doubler methods ; 7.3. Repair analysis for crack-line damages ; 7.3.1. Wang and Rose's crack bridging model ; 7.3.2. Two-stage analysis procedure for crack patching ; 7.4. Patch design for an elliptical damage ; 7.4.1. Design criteria and guidelines ; 7.4.2. Patch design algorithm 7.5. Summary ; References ; Chapter 8. Design and optimization of scarf repairs ; 8.1. Introduction ; 8.2. Residual strength of scarfed laminates ; 8.2.1. Tension and compression loading ; 8.2.2. Predictive modeling ; 8.3. Shape optimization of scarf repairs ; 8.3.1. Assessment of existing shaping methods 8.3.2. Optimum solution ; 8.3.3. Case studies ; 8.4. Structural doublers ; References -- Part 2. Manufacturing and inspection. Chapter 9. Repair manufacturing processes ; 9.1. Introduction ; 9.2. Scarfing operation ; 9.3. Repair patch manufacturing ; 9.3.1. Soft patch ; 9.3.2. Molded patch ; 9.4. Surface treatment ; 9.5. Adhesive bonding ; 9.6. Repair of thick laminates ; References ; Chapter 10. Non-destructive evaluation of bond ; 10.1. Introduction ; 10.2. Detection of disbonds ; 10.3. Detection of weak adhesion bonds ; 10.4. Local bond proof testing ; 10.5. Satellite coupon proof test ; References ; Index. |
| Record Nr. | UNINA-9910955411203321 |
Wang Chun Hui
|
||
| Saint Louis, : Elsevier Science, 2015 | ||
| Lo trovi qui: Univ. Federico II | ||
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Composite structures, design, safety, and innovation [e-book] / B.F. Backman
| Composite structures, design, safety, and innovation [e-book] / B.F. Backman |
| Autore | Backman, Bjorn F. |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Amsterdam ; Boston, Mass. : Elsevier, 2005 |
| Descrizione fisica | x, 244 p. : ill. ; 25 cm |
| Disciplina | 629.13431 |
| Soggetto topico |
Airframes - Materials
Composite materials Airframes - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN |
9780080445458
0080445454 |
| Formato | Risorse elettroniche |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1.0Introduction -- 2.0Structural Design -- 3.0Structural Safety -- 4.0Innovation -- 5.0Safety Objectives -- 6.0Risk Management -- 7.0Trades -- 8.0Building Block Approach -- 9.0Design Scenarios -- 10.0The Design Process -- 11.0Damage and Detection -- 12.0Design Philosophy -- 13.0Analysis of Design Criteria -- 14.0Design Example -- 15.0Design of Composite Structure -- Appendix AA Model of Ultimate Integrity -- Appendix BA Comparison between Metal and Composite Panels |
| Record Nr. | UNISALENTO-991003228409707536 |
Backman, Bjorn F.
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||
| Amsterdam ; Boston, Mass. : Elsevier, 2005 | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Mechanics of aero-structures / Sudhakar Nair
| Mechanics of aero-structures / Sudhakar Nair |
| Autore | Nair, Sudhakar, 1944- |
| Descrizione fisica | xii, 182 pages : ill. ; 27 cm |
| Disciplina | 629.132 |
| Soggetto topico |
Airframes - Design and construction
Aerodynamics |
| ISBN | 9781107075771 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991003609439707536 |
Nair, Sudhakar, 1944-
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||
| Lo trovi qui: Univ. del Salento | ||
| ||
Notes on the design of latticed columns subject to lateral loads / / by Charles J. McCarthy
| Notes on the design of latticed columns subject to lateral loads / / by Charles J. McCarthy |
| Autore | McCarthy Charles J. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1922 |
| Descrizione fisica | 1 online resource (18 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airframes - Design and construction
Lateral loads Lattice theory |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713374003321 |
McCarthy Charles J.
|
||
| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1922 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter
| Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
| Descrizione fisica | 1 online resource (555 p.) |
| Disciplina |
629.134/31
629.1 s |
| Altri autori (Persone) |
MurthyS. N. B
PaynterGerald C |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Airframes - Design and construction
Airplanes - Motors |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-576-3
1-60086-357-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation""
""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration"" ""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" |
| Record Nr. | UNINA-9910457214703321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter
| Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
| Descrizione fisica | 1 online resource (555 p.) |
| Disciplina |
629.134/31
629.1 s |
| Altri autori (Persone) |
MurthyS. N. B
PaynterGerald C |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Airframes - Design and construction
Airplanes - Motors |
| ISBN |
1-60086-576-3
1-60086-357-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation""
""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration"" ""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" |
| Record Nr. | UNINA-9910781405503321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax
| Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax |
| Autore | Lomax Ted L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 |
| Descrizione fisica | 1 online resource (297 p.) |
| Disciplina | 629.134/31 |
| Collana | AIAA education series |
| Soggetto topico |
Airframes - Design and construction
Structural dynamics Transport planes - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-246-2
1-60086-118-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""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 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""; ""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"" ""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"" |
| Record Nr. | UNINA-9910457218703321 |
Lomax Ted L
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||