Get Aircraft Aerodynamic Design: Geometry and Optimization PDF

By András Sóbester, Alexander I J Forrester

ISBN-10: 0470662573

ISBN-13: 9780470662571

Optimal airplane layout is most 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 diverse candidate airframe shapes based on alterations within the values of those variables. This model's goals are to be versatile and concise, and in a position to yielding quite a lot of shapes with a minimal variety of layout variables. in addition, the method of changing those variables into airplane geometries has to be strong. regrettably, flexibility, conciseness and robustness can seldom be accomplished simultaneously.

Aircraft Aerodynamic layout: Geometry and Optimization addresses this challenge by means of navigating the sophisticated trade-offs among the competing pursuits of geometry parameterization. It beginswith the basics of geometry-centred airplane layout, through a overview of the development blocks of computational geometries, the curve and floor formulations on the middle of plane geometry. The authors then conceal quite a number legacy formulations within the build-up in the direction of a dialogue of the main versatile form versions utilized in aerodynamic layout (with a spotlight on elevate producing surfaces). The booklet takes a realistic process and contains MATLAB®, Python and Rhinoceros® code, in addition to ‘real-life’ instance case studies.

Key features: 

  • Covers powerful geometry parameterization in the context of layout optimization
  • Demonstrates how geometry parameterization is a crucial component of smooth plane design
  • Includes code and case reviews which permit the reader to use every one theoretical idea both as an reduction to knowing or as a development block in their personal geometry model
  • Accompanied through an internet site web hosting codes

Aircraft Aerodynamic layout: Geometry and Optimization is a realistic 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

Given the simple, analytical test function, this was a barely noticeable minor inconvenience for this simple problem, the search taking a few minutes, as opposed to a second or two in stages 1 and 2. However, the increase would have been immensely inconvenient if a high-fidelity numerical analysis process (perhaps involving multiple disciplines) had been needed to compute the objective. Also, this geometry now has a blemish: the cusp between the two lobes is nowhere near the cabin floor level – this is likely to be a structurally inefficient solution.

These starting geometries should fill the design space relatively uniformly, increasing the probability that we exploit the neighbourhoods of all radically different designs. If the cost of computing the objective function is relatively low and the number of design variables is high, evolutionary optimization methods can make very efficient global optimizers. A large range of such methods is available, all sharing the fundamental philosophy of imitating the mechanics of natural evolution. Natural life results from the nonrandom survival of randomly varying replicators – in evolutionary optimizers (such as genetic algorithms, which are the best known representative of this class), encoded versions of design variable strings take the role of the replicators, and the objective function, through some artificial selection scheme, determines survival (or loss) of candidate geometries.

From the flow conditions and the overall estimated weight of the aeroplane we can compute the required aerofoil lift coefficient cl , so we can perform an iterative flow analysis around each candidate design until we find the angle of attack that yields that target cl . A simple (low-level) efficiency objective can then be the drag coefficient obtained at that angle of attack. A suitable aerofoil shape parameterization needs to be identified next (we will consider plenty of options for this in Chapters 6 and 7), as well as a 2D viscous flow simulation code capable of the calculation outlined above (a simple 2D panel code with viscous boundary layer, implemented in MATLAB® and Python is included in the toolkit accompanying this book, and is employed in the human-powered aircraft case study in Chapter 12).

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

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