Refinement and analysis of concept

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航空宇航学院 Refinement of Landing Gear • The main points to be investigated are – Overall layout geometry, including the number of main gear units – Number and size of the wheels/tyres – Location of suitable stowage volume – Location of suitable load attachment points. • Clearly these latter two issues are closely related to the layout of the structural members. See Addendum 1 for more detail Aircraft Conceptual Design
Fuselage Layout 航空宇航学院 • A more precise and detailed layout of the fuselage may now be undertaken. – Influence of the wing junction with the fuselage – Landing gear attachment and stowage – Layout of the cockpit region, windscreen geometry, etc. – Detail of the powerplant installation – Payload detail • Doors,windows • Freight loading access and doors – Special detail considerations With an aid of CAD software 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 and 6: 航空宇航学院 Refinements of P
Page 7 and 8: Powerplant Location • Installatio
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: 航空宇航学院 An example of st
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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