General Aviation Aircraft Design: Applied Methods and ProceduresButterworth-Heinemann, 3.9.2013 - 1048 sivua Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design.
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Sisältö
1 | |
33 | |
55 | |
77 | |
97 | |
Chapter 6 Aircraft Weight Analysis | 133 |
Chapter 7 Selecting the Power Plant | 181 |
Chapter 8 The Anatomy of the Airfoil | 235 |
15 Aircraft Drag Analysis | 661 |
Chapter 16 Performance Introduction | 761 |
Chapter 17 Performance TakeOff | 791 |
Chapter 18 Performance Climb | 821 |
Chapter 19 Performance Cruise | 847 |
Chapter 20 Performance Range Analysis | 895 |
Chapter 21 Performance Descent | 925 |
Chapter 22 Performance Landing | 935 |
Chapter 9 The Anatomy of the Wing | 299 |
Chapter 10 The Anatomy of Lift Enhancement | 401 |
Chapter 11 The Anatomy of the Tail | 459 |
Chapter 12 The Anatomy of the Fuselage | 521 |
Chapter 13 The Anatomy of the Landing Gear | 547 |
Chapter 14 The Anatomy of the Propeller | 581 |
Chapter 23 Miscellaneous Design Notes | 947 |
Appendix A Atmospheric Modeling | 985 |
Appendix B The Aerospace Engineers Formula Sheet | 997 |
1007 | |
Muita painoksia - Näytä kaikki
General Aviation Aircraft Design: Applied Methods and Procedures Snorri Gudmundsson Esikatselu ei käytettävissä - 2013 |
General Aviation Aircraft Design: Applied Methods and Procedures Snorri Gudmundsson Esikatselu ei käytettävissä - 2013 |
General Aviation Aircraft Design: Applied Methods and Procedures Snorri Gudmundsson Esikatselu ei käytettävissä - 2016 |
Yleiset termit ja lausekkeet
aerodynamic aileron Aircraft Design airfoil airplane airspeed altitude analysis angle aspect ratio assuming aviation blade boundary layer calculated CDmin chord Cirrus SR22 climb CLmax configuration deflection density Derivation of Equation Determine drag coefficient effect estimate example factor feature flap flight force ft/s or m/s fuel fuselage geometry graph gross weight horizontal tail increase induced drag KCAS KTAS laminar landing gear leading edge lift coefficient lift curve slope lift-induced drag load Mach number manufacturing method minimum drag NACA operation PBHP pilot piston engine pitch pitching moment planform pressure propeller efficiency radians range reduce reference Reynolds number rotation section lift coefficients selected shown in Figure skin friction spanwise spar stability stalling speed Step structure surface Table thrust tion trailing edge turboprop typical V-tail vertical tail wing area winglet wingtip