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Titlebook: Conceptual Shape Optimization of Entry Vehicles; Applied to Capsules Dominic Dirkx,Erwin Mooij Book 2017 Springer International Publishing

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發(fā)表于 2025-3-21 16:25:43 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書(shū)目名稱Conceptual Shape Optimization of Entry Vehicles
副標(biāo)題Applied to Capsules
編輯Dominic Dirkx,Erwin Mooij
視頻videohttp://file.papertrans.cn/236/235034/235034.mp4
概述The joint discussion of the relevant aspects of flight dynamics, aerothermodynamics, shape modelling and optimization in a single comprehensive text provides a crucially valuable reference for concept
叢書(shū)名稱Springer Aerospace Technology
圖書(shū)封面Titlebook: Conceptual Shape Optimization of Entry Vehicles; Applied to Capsules Dominic Dirkx,Erwin Mooij Book 2017 Springer International Publishing
描述.This book covers the parameterization of entry capsules, including Apollo capsules and planetary probes, and winged entry vehicles such as the Space Shuttle and lifting bodies. The aerodynamic modelling is based on a variety of panel methods that take shadowing into account, and it has been validated with flight and wind tunnel data of Apollo and the Space Shuttle. The shape optimization is combined with constrained trajectory analysis, and the multi-objective approach provides the engineer with a Pareto front of optimal shapes. ..The method detailed in .Conceptual Shape Optimization of Entry Vehicles .is straightforward, and the output gives the engineer insight in the effect of shape variations on trajectory performance. All applied models and algorithms used are explained in detail, allowing for reconstructing the design tool to the researcher’s requirements. ..Conceptual Shape Optimization of Entry Vehicles. will be of interest to both researchers and graduate students in the field of aerospace engineering, and to practitioners within the aerospace industry. .
出版日期Book 2017
關(guān)鍵詞Atmospheric entry; Multi-objective shape optimization; Local-inclination methods; Hypersonic aerothermo
版次1
doihttps://doi.org/10.1007/978-3-319-46055-0
isbn_softcover978-3-319-83430-6
isbn_ebook978-3-319-46055-0Series ISSN 1869-1730 Series E-ISSN 1869-1749
issn_series 1869-1730
copyrightSpringer International Publishing Switzerland 2017
The information of publication is updating

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Aerothermodynamics,erodynamic forces and moments, and the heat flux are crucial parameters driving the vehicle performance. Modelling the aerothermodynamic properties of re-entry vehicles is a highly complicated and multidisciplinary problem. For conceptual design optimization, incorporating a high-fidelity analysis i
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Numerical Interpolation,hicle surface from these points requires an interpolation algorithm. In this work, we use cubic splines and spline surfaces as the interpolation scheme. In this chapter the basics of these methods, as well as some issues pertaining to their implementation, are discussed. The splines and spine surfac
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Vehicle Geometry,hods by which we parameterize these vehicle shape, e.g. the manner in which we relate the shape parameters that are to be optimized to a continuous vehicle shape. The capsule is defined by a combination of basic geometric shapes: sphere segments, a torus segment and a conical frustum. The winged veh
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Optimization,hm. In this chapter, we start by discussing the general problem of both single- and multi-objective global optimization, followed by a discussion of the PSO method, including the approach we use to for multi-objective optimality and constraint handling. Finally, we show how the optimization algorith
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1869-1730 ive text provides a crucially valuable reference for concept.This book covers the parameterization of entry capsules, including Apollo capsules and planetary probes, and winged entry vehicles such as the Space Shuttle and lifting bodies. The aerodynamic modelling is based on a variety of panel metho
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