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Aerodynamic Design of Transport Aircraft [Pehme köide]

  • Formaat: Paperback / softback, 656 pages
  • Ilmumisaeg: 29-Apr-2025
  • Kirjastus: IOS Press,US
  • ISBN-10: 1586039709
  • ISBN-13: 9781586039707
Teised raamatud teemal:
  • Formaat: Paperback / softback, 656 pages
  • Ilmumisaeg: 29-Apr-2025
  • Kirjastus: IOS Press,US
  • ISBN-10: 1586039709
  • ISBN-13: 9781586039707
Teised raamatud teemal:
The origin of Aerodynamic Design of Transport Aircraft stems from the time when the author was appointed part-time professor in the Aerospace Faculty of Delft University of Technology. At the time his main activities were those of leading the departments of Aerodynamics, Performance and Preliminary Design at Fokker Aircraft Company. The groundwork for this book started in 1987 as a series of lecture notes consisting mainly of pictorial material with a minimum of English explanatory text. After the demise of Fokker in 1996 one feared that interest in aeronautical engineering would strongly diminish. As a result of this, the course was discontinued and the relationship between the author and the faculty came to an end. Two years later the situation was reappraised, and the interest in aeronautical engineering remained, so the course was reinstated with a former Fokker colleague Ronald Slingerland as lecturer. The lecture notes from these courses form the foundation of this publication.
Notations xiii
Part 1 - Introduction
Introduction
3(4)
Classification of fixed-wing aircraft
7(4)
Design requirements and objectives of transport aircraft
11(2)
The aircraft design process
13(16)
Geometry
29(2)
Design of the external geometry
31(4)
Computing velocity and pressure distributions on fixed bodies in attached flow conditions
35(2)
The limitations of boundary layer theories
37(2)
Computations with separated flow
39(4)
Part 2 - Pressure Distributions
The relation between supervelocity and pressure coefficient
43(4)
The relation between geometry and pressure distribution
47(2)
Pressure distributions on components which are not required to generate aerodynamic forces
49(20)
Pressure distributions on components which are required to generate aerodynamic forces
69(2)
Pressure distributions on wings
71(4)
Part 3 - Airfoils
The Pressure distribution on airfoil sections
75(30)
The advantages of supercritical airfoil sections in comparison to sonic-rooftop sections
105(2)
The buffet onset boundary and beyond
107(6)
Reynolds number effects on section characteristics at high Mach numbers
113(6)
Low-speed stalling characteristics of airfoil sections
119(16)
Part 4 - Swept Wings
The development of the swept-wing concept
135(32)
The first generation of swept-wing aircraft
167(10)
Root and tip effects on swept wings
177(16)
Design considerations regarding the pressure distribution on finite wings
193(4)
Examples of actual wing designs for high-speed transport aircraft
197(80)
Part 5 - Low-Speed Aerodynamic Limits
The maximum lift coefficient of airfoil sections equipped with high-lift devices
277(38)
The maximum lift coefficient and the stalling characteristics of full-scale aircraft
315(28)
The lift-drag ratio in take-off and landing
343(26)
Part 6 - High-Speed Aerodynamic Limits
The buffet onset boundary
369(8)
Flight characteristics between MMO and MD
377(12)
Part 7 - Stability And Control
Tail surface design
389(4)
The horizontal tail surface
393(20)
The vertical tail surface
413(10)
Control surface design
423(10)
Lift spoiling control surfaces (spoiler panels)
433(8)
Control surface actuation
441(12)
Propeller slipstream effects
453(26)
Part 8 - Engine Integration
Engine intakes
479(20)
Engine exhausts
499(10)
Thrust reversers
509(12)
Part 9 - Aircraft Performance
Subsonic cruise drag
521(30)
Breguet's range equation
551(6)
Aircraft weight
557(30)
Part 10 - Safety And Regulations
Certification regulations and design rules
587(8)
Take-off performance regulations
595(14)
Flight safety in civil aviation
609(12)
Sources 621