Aircraft Aerodynamic Design: Geometry and Optimization by András Sóbester, Alexander I J Forrester

By András Sóbester, Alexander I J Forrester

Optimal plane layout is very unlikely with out a parametric illustration of the geometry of the airframe. we'd like a mathematical version built with a suite of controls, or layout variables, which generates diversified candidate airframe shapes in accordance with alterations within the values of those variables. This model's pursuits are to be versatile and concise, and in a position to yielding a variety of shapes with a minimal variety of layout variables. additionally, the method of changing those variables into plane geometries has to be powerful. lamentably, flexibility, conciseness and robustness can seldom be accomplished simultaneously.

Aircraft Aerodynamic layout: Geometry and Optimization addresses this challenge through navigating the sophisticated trade-offs among the competing targets of geometry parameterization. It beginswith the basics of geometry-centred airplane layout, via a evaluation of the development blocks of computational geometries, the curve and floor formulations on the middle of airplane geometry. The authors then hide more than a few legacy formulations within the build-up in the direction of a dialogue of the main versatile form types utilized in aerodynamic layout (with a spotlight on raise producing surfaces). The e-book takes a realistic technique and comprises MATLAB®, Python and Rhinoceros® code, in addition to ‘real-life’ instance case studies.

Key features: 

  • Covers potent geometry parameterization in the context of layout optimization
  • Demonstrates how geometry parameterization is a vital part of glossy plane design
  • Includes code and case reports which permit the reader to use each one theoretical inspiration both as an relief to figuring out or as a construction block in their personal geometry model
  • Accompanied through an internet site internet hosting codes

Aircraft Aerodynamic layout: Geometry and Optimization is a pragmatic consultant for researchers and practitioners within the aerospace undefined, and a reference for graduate and undergraduate scholars in plane layout and multidisciplinary layout optimization.

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Extra resources for Aircraft Aerodynamic Design: Geometry and Optimization

Sample text

For instance, specific fuel consumption might be a key parameter in gas turbine engine design, but it is not a design variable. Nor is bypass ratio a design variable in the sense of the geometry-centred design processes we are dealing with here, though – scope for more confusion – the first, conceptual, non-geometric phase of the design of a turbofan engine might well view bypass ratio as a design variable. A simple test to apply to a set of parameters related to a design, which might determine whether they are higher level metrics or design variables (or a mixture), is to consider what would happen if several engineers were issued with these sets of parameters and their unambiguous definitions and they were told to come up, working independently, with the corresponding design blueprints.

The goal of the exercise is therefore to wrap these markers with the ‘tightest’ possible cross-section curve. In what follows we shall take a three-stage approach to solving this problem, gradually ramping up the flexibility of the cross-section geometry. Stage 1: A Circle From a purely structural standpoint, the most efficient shape for a slender pressure vessel is a cylinder with hemispherical end caps. As a result, a large proportion of aircraft with pressurized cabins feature a fuselage with a circular cross-section.

In Chapter 9 we shall discuss the construction of 3D wings in the same spirit, building upon the parameterization of aerofoil cross-sections (Chapters 5, 6 and 7) – analogous to the fuselage cross-sections here – and planforms (Chapter 8), analogous to the side profile definition of the fuselage in this chapter. 6 Necessary Flexibility One of the key themes running through this book is the control of the dimensionality of a parametric geometry – that is, how we make sure that the desire for flexibility does not render the geometrical formulation completely unusable in an optimization context.

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