Aircraft Design: A Conceptual ApproachThis textbook for advanced students focuses on industry design practice rather than theoretical definitions. Covers configuration layout, payload considerations, aerodynamics, propulsion, structure and loads, weights, stability, and control, performance, and cost analysis. Annotation copyright Book |
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Page 5
... Chapter 1 . 1.1 1.2 3 Chapter 2 . 2.1 2.2 2.3 11 Chapter 3 . 3.1 3.2 3.3 Overview of the Design Process Introduction Phases of Aircraft Design Aircraft Conceptual Design Process Sizing from a Conceptual Sketch Introduction Takeoff ...
... Chapter 1 . 1.1 1.2 3 Chapter 2 . 2.1 2.2 2.3 11 Chapter 3 . 3.1 3.2 3.3 Overview of the Design Process Introduction Phases of Aircraft Design Aircraft Conceptual Design Process Sizing from a Conceptual Sketch Introduction Takeoff ...
Page 7
... Chapter 14. Structures and Loads Introduction Loads Categories Air Loads Inertial Loads Power - Plant Loads 14.1 ... Chapter 15. Weights Introduction Approximate Group Weights Method 407 451 15.1 15.2 15.3 Statistical Group Weights ...
... Chapter 14. Structures and Loads Introduction Loads Categories Air Loads Inertial Loads Power - Plant Loads 14.1 ... Chapter 15. Weights Introduction Approximate Group Weights Method 407 451 15.1 15.2 15.3 Statistical Group Weights ...
Page 11
... Chapters 2 and 3 provide an overall introduction to the design process . Chapter 2 discusses how the conceptual design process works , and how it fits into the overall process of aircraft development . Chapter 3 presents a " first ...
... Chapters 2 and 3 provide an overall introduction to the design process . Chapter 2 discusses how the conceptual design process works , and how it fits into the overall process of aircraft development . Chapter 3 presents a " first ...
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Common terms and phrases
actual aerodynamic aerodynamic center aileron aircraft design aircraft weight airflow airfoil altitude analysis angle of attack approximately aspect ratio calculated camber canard Chapter chord climb component compression Conceptual Approach conceptual design cost cross section cruise curve deflection determined dihedral duct effect empty weight engine equations estimated fighter flap flight flow force ft² fuel fuselage horizontal tail increase induced drag initial inlet landing gear layout leading edge leading-edge lift coefficient load factor loiter longitudinal Mach number maximum lift methods MISSION SEGMENT NACA nacelle nozzle parasite drag payload pilot pitching pitching moment produce propeller propulsion reduced roll shear shock shown in Fig sizing speed stall static structural subsonic supersonic surface T-tail takeoff weight thrust transonic turbofan turboprop turn rate typical vectoring velocity vertical tail VTOL wave drag weight fraction wetted area wheel wing loading zero