Synthesis of Subsonic Airplane Design: An introduction to the preliminary design of subsonic general aviation and transport aircraft, with emphasis on layout, aerodynamic design, propulsion and performance

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Springer Science & Business Media, 29 Ιουν 2013 - 598 σελίδες
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Since the education of aeronautical engineers at Delft University of Technology started in 1940 under tae inspiring leadership of Professor H.J. van der Maas, much emphasis has been placed on the design of aircraft as part of the student's curriculum. Not only is aircraft design an optional subject for thesis work, but every aeronautical student has to carry out a preliminary airplane design in the course of his study. The main purpose of this preliminary design work is to enable the student to synthesize the knowledge ob tained separately in courses on aerodynamics, aircraft performances, stability and con trol, aircraft structures, etc. The student's exercises in preliminary design have been directed through the years by a number of staff members of the Department of Aerospace Engineering in Delft. The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years. Not only has he acquired vast experience in teaching airplane design at university level, but he has also been deeply involved in design-oriented re search, e.g. developing rational design methods and systematizing design information. I am very pleased that this wealth of experience, methods and data is now presented in this book.
 

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Περιεχόμενα

THE GENERAL ARRANGEMENT
27
forces
29
FUSELAGE DESIGN
61
Designation of Federal Airways Controlled Airspace and Reporting Points
71
AN APPRECIATION OF SUBSONIC ENGINE TECHNOLOGY
97
AIR CARRIERS AIR TRAVEL CLUBS AND OPERATORS
123
DESIGN FOR PERFORMANCE
141
Of interest only
157
APPENDIX B THE COMPUTATION OF CIRCUMFERENCES AREAS AND VOLUMES OF CURVES
445
THE WEIGHT PENALTY METHOD FOR FUSELAGE STRUCTURAL WEIGHT PREDICTION
457
References
465
E5 Pitching moment of the wing
476
APPENDIX F PREDICTION OF THE AIRPLANE POLAR AT SUBCRITICAL SPEEDS IN
487
F5 Protuberances surface imperfections and other extras
512
References
519
APPENDIX G PREDICTION OF LIFT AND DRAG IN THE LOWSPEED CONFIGURATION
525

Beyond the scope of this book
171
CHOICE OF THE ENGINE AND PROPELLER AND INSTALLATION OF THE POWERPLANT
181
AN INTRODUCTION TO WING DESIGN
215
Table 12 Subdivision of FAR requirements
246
AIRPLANE WEIGHT AND BALANCE
263
PRELIMINARY TAILPLANE DESIGN
303
THE UNDERCARRIAGE LAYOUT
341
ANALYSIS OF AERODYNAMIC AND OPERATIONAL CHARACTERISTICS
365
EVALUATION AND PRESENTATION OF A PRELIMINARY DESIGN
389
REFERENCES
401
APPENDIX A DEFINITIONS RELATING TO THE GEOMETRY AND AERODYNAMIC CHARACTERISTICS
435
References
443
G3 Lift of aircraft with deflected trailingedge flaps
537
note the follow
538
G4 Prediction of the lowspeed drag polar
543
G6 Drag due to extension of a retractable undercarriage
550
References
556
H1 Scope of the method
563
H4 Specific performance of turbofan engines
565
APPENDIX J PRINCIPAL DATA OF THE US AND ICAO STANDARD ATMOSPHERES
571
K3 Procedure for determining the takeoff field length
578
References
586
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