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 PerformanceSpringer Netherlands, 1976 - 598 σελίδες Since the education of aeronautical engineers at Delft University of Technology started in 1940 under the 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. |
Περιεχόμενα
GENERAL ASPECTS OF AIRCRAFT CONFIGURATION DEVELOPMENT | 1 |
THE GENERAL ARRANGEMENT | 27 |
forces | 29 |
Πνευματικά δικαιώματα | |
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Άλλες εκδόσεις - Προβολή όλων
Synthesis of Subsonic Airplane Design: An introduction to the preliminary ... E. Torenbeek Περιορισμένη προεπισκόπηση - 2013 |
Synthesis of Subsonic Airplane Design: An introduction to the preliminary ... Egbert Torenbeek Περιορισμένη προεπισκόπηση - 1982 |
Synthesis of Subsonic Airplane Design: An introduction to the preliminary ... Egbert Torenbeek Δεν υπάρχει διαθέσιμη προεπισκόπηση - 2010 |
Συχνά εμφανιζόμενοι όροι και φράσεις
aerodynamic airfoil airplane airworthiness altitude angle of attack approximately aspect ratio blade Boeing bypass ratio cabin characteristics chord climb condition configuration cruising flight deflection drag coefficient effect efficiency empty weight engine failure estimation factor field length flap flow fuel consumption fuselage gine given high-lift devices high-speed increase increment induced drag inlet installation jet engine landing gear layout leading edge lift coefficient limited Mach number maximum lift method minimum MTOW NACA nacelle noise operational optimum parameter passenger payload performance pitch pitching moment prediction preliminary design pressure ratio profile drag propeller propulsive reduced relative result SAE Paper seats Section shape slotted specific fuel consumption speed stability stall structure weight subsonic swept wings tail tailplane takeoff weight tion transport aircraft turbine turboprop undercarriage wetted area wing area wing loading