Refinement and analysis of concept

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Powerplant Location • Versatility and access: 航空宇航学院 – As a general rule engines mounted in pods or nacelles on the outside of the aircraft are more versatile than those buried within the airframe. – It is usually possible to accommodate different engines without too much difficulty, thereby more readily handling upgrades or specific customer requirements. – Podded and nacelle-mounted engines are also preferable for maintenance since access is generally more direct and need not involve significant structural penalties. – Also air intakes and exhausts are usually shorter and can be more efficient. Aircraft Conceptual Design
Powerplant Location • Installation clearance 航空宇航学院 – As the engine dimensions are defined it is necessary to check installation clearances, such as propeller tip spacing from adjacent structure or the ground and under-wing nacelle ground clearance on a low wing aircraft. Aircraft Conceptual Design
Page 1 and 2: Refinement and Analysis of Design C
Page 3 and 4: Introduction 航空宇航学院 •
Page 5: 航空宇航学院 Refinements of P
Page 9 and 10: Powerplant Location • Acoustic co
Page 11 and 12: Powerplant Location • Powerplant/
Page 13 and 14: • High lift device Refinement of
Page 15 and 16: 航空宇航学院 Refinement of ae
Page 17 and 18: 航空宇航学院 Refinement of co
Page 19 and 20: Wing structure layout 航空宇航
Page 21 and 22: 航空宇航学院 An example of st
Page 23 and 24: Fuselage Layout 航空宇航学院
Page 25 and 26: 航空宇航学院 Mass Prediction
Page 27 and 28: Aerodynamic Analysis Theoretical +
Page 29 and 30: Performance Analysis 航空宇航
Page 31 and 32: Cost Analysis 航空宇航学院 Co
Page 33 and 34: • What is first cost First cost
Page 35 and 36: 航空宇航学院 Direct Operating
Page 37 and 38: Introduction to AAA software A soft
Page 39 and 40: Finally, we use optimization to sea
Page 41 and 42: Output of the Preliminary Design
Page 43 and 44: Fwd FA Seat (View Fwd) 航空宇航
Page 45: A overall layout (AD-400) 航空宇

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