Applied Computational Aerodynamics. için kapak resmi
Applied Computational Aerodynamics.
Başlık:
Applied Computational Aerodynamics.
Yazar:
Henne, P. A.
ISBN:
9781600863790
Yazar Ek Girişi:
Fiziksel Tanımlama:
1 online resource (926 pages)
Seri:
Progress in Astronautics and Aeronautics ; v.125

Progress in Astronautics and Aeronautics
İçerik:
Cover -- Title -- Copyright -- Table of Contents -- Preface -- Part 1. History -- Chapter 1. The Panel Method: Its Original Development -- Introduction -- Getting into the Problem -- Preliminary Work -- Getting on to the Method -- Trying to Solve the Equations -- The Solution -- Programming and First Results -- Other Early Extensions -- Four Key Helpers -- References -- Bibliography -- Part 2. Computational Aerodynamic Schemes -- Chapter 2. Linear Potential Schemes -- Introduction -- Mapping Solutions -- Panel Method Singularity Distribution -- Higher-Order Singularities -- Boundary Conditions -- Matrix Solutions -- References -- Chapter 3. Full-Potential, Euler, and Navier-Stokes Schemes -- Introduction -- Mathematical Models of Fluid Flow -- Algorithms for Potential Flow -- Algorithms for the Euler Equations -- Viscous Flow Calculations -- Conclusion -- References -- Chapter 4. Grid-Generation Methodology in Applied Aerodynamics -- Introduction -- Domain Discretization Ideas -- Basic Grid-Generation Methods -- Applications -- Summary -- References -- Part 3. Airfoils, Wings, and Wing Bodies -- Chapter 5. Subsonic Airfoil Design -- Introduction -- Methods of Solution: A Brief Historical Perspective -- Viscosity and the Airfoil Design Problem -- High-Lift Airfoil Development -- Generalized Airfoil Design Capability -- Example Airfoil Designs -- Closing Remarks -- References -- Chapter 6. Elements of Airfoil Design Methodology -- Introduction -- Airfoil Design -- Viscous Analysis Methods -- Inverse Methods -- Integrated Analysis/Design System -- Conclusions -- References -- Chapter 7. Inverse Airfoil Design: A Classical Approach Updated for Transonic Applications -- Introduction -- Formulation of the Inverse Design Problem -- Transonic Flowfield Solution -- Contour Modification -- Constraints in Incompressible Flow.

An Alternate Look at the Constraints -- Enforcement of Constraints -- Results -- Summary -- References -- Chapter 8. Innovation with Computational Aerodynamics: The Divergent Trailing-Edge Airfoil -- Introduction -- Origin of the Concept -- Development of the DTE Airfoil Concept -- New Wing Application of DTE Airfoils -- Derivative Wing Application of DTE Airfoils -- Summary -- References -- Chapter 9. Euler and Potential Computational Results for Selected Aerodynamic Configurations -- Nomenclature -- Introduction -- Commercial Transport Wing/Body Configurations -- Generic Fighter -- Delta Wing -- References -- Part 4. High-Lift Systems -- Chapter 10. Computational Aerodynamics Applied to High-Lift Systems -- Nomenclature -- Introduction -- Two-Dimensional Airfoil Methods -- Three-Dimensional Methods -- Some Applications of Computational High-Lift Design Methodology -- References -- Chapter 11. Development of High-Lift Wing Modifications for an Advanced Capability EA-6B Aircraft -- Introduction -- EA-6B High-Lift Wing Modification -- Computational Techniques -- Computational Design Problem -- Summary -- Concluding Remarks -- References -- Part 5. Propulsion Systems -- Chapter 12. Navier-Stokes Methods for Internal and Integrated Flow Prediction -- The Problem -- Available Technology -- Coupled External/Internal Flow -- Assessment -- References -- Chapter 13. Computational Analysis of Rotor-Stator Interaction in Turbomachinery Using Zonal Techniques -- Introduction -- Integration Schemes -- Zonal Boundary Conditions -- Natural Boundary Conditions -- Results -- Areas of Current and Future Research -- Summary -- References -- Part 6. Rotors -- Chapter 14. Euler/Navier-Stokes Computations of the Flowfield of a Helicopter Rotor in Hover and Forward Flight -- Introduction -- Governing Equations -- Finite-Volume Method -- Time-Stepping Scheme.

Boundary Conditions -- Computed Examples -- Conclusions -- References -- Part 7. Complex Configurations -- Chapter 15. CFD Applications to Complex Configurations: A Survey -- Introduction -- General Aircraft Characteristics -- Viscous Effects on General Configurations -- Wakes and Flowfields -- Engine Airframe Integration -- Concluding Remarks -- References -- Chapter 16. Computational Aerodynamics Applied to General Aviation/Business Aircraft -- Introduction -- Geometry: The First Hurdle -- Computational Aerodynamics Usage -- Applications -- Computational Aerodynamics Challenges -- Future Directions -- References -- Chapter 17. Application of Computational Fluid Dynamic Methods to the Component Aerodynamic Design of the V-22 Osprey Tilt Rotor Vehicle -- Nomenclature -- Introduction -- Objective -- Aerodynamic Design of the Blade Sections -- Aerodynamic Design of the Wing/Flap Section -- Additional CFD Successes on the V-22 -- Concluding Remarks -- References -- Chapter 18. Aerodynamic Analysis Using Euler Equations: Capabilities and Limitations -- Introduction -- Basic Features of TEAM -- Analysis Results -- Concluding Remarks -- References -- Chapter 19. Toward the Routine Aerodynamic Analysis of Complex Configurations -- Introduction -- PanAir: Applications -- TranAir: Description -- TranAir: Applications -- Future Directions -- Closing Remarks -- References -- Chapter 20. Computational Aerodynamic Simulation Experience -- Nomenclature -- Introduction -- Discussion -- Conclusions -- References -- Chapter 21. Navier-Stokes Computations About Complex Configurations Including a Complete F-16 Aircraft -- Introduction -- Governing Equations and Numerical Approach -- Zonal-Grid Approach -- Data Management -- NACA 0012 Wing Results -- Wing C Results -- F-16A Results -- Conclusions -- References.

Chapter 22. Computational Fluid Dynamics Design Applications at Supersonic/Hypersonic Speeds -- Introduction -- Case 1: Hypersonic Vehicle Design and Integration -- Case 2: Sonic Boom -- Case 3: Supersonic Laminar Flow Control and Drag Due to Lift -- Case 4: High Mach Engine Inlet Design -- Conclusions, Implications, Perspective on CFD Applications in the Future -- References -- Chapter 23. Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations -- Introduction -- Governing Equations -- Solution Methodology -- Capabilities and Applications -- Conclusions -- References -- Chapter 24. Flow Computations for the Space Shuttle in Ascent Mode Using Thin-Layer Navier-Stokes Equations -- Introduction -- Computational Procedure -- Results -- Concluding Remarks -- References -- Part 8. Forecast -- Chapter 25. Future Directions for Applied Computational Fluid Dynamics -- Introduction -- Design Applications -- Mature CFD Capability -- CFD Validation -- Challenges for the Future -- References -- Epilogue -- Author Index for Volume 125.
Notlar:
Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2017. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
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