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Titlebook: Handbook of Numerical Simulation of In-Flight Icing; Wagdi George Habashi Living reference work 20200th edition In-Flight Icing.Computati

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书目名称Handbook of Numerical Simulation of In-Flight Icing
编辑Wagdi George Habashi
视频video
概述Assembles and cross-references an unrivaled selection of competencies and best practices on in-flight icing.Clarifies and brings attention to efforts promoting simulation for certifying aircraft to fl
图书封面Titlebook: Handbook of Numerical Simulation of In-Flight Icing;  Wagdi George Habashi Living reference work 20200th edition  In-Flight Icing.Computati
描述.This Handbook of Numerical Simulation of In-Flight Icing covers an array of methodologies and technologies on numerical simulation of in-flight icing and its applications. Comprised of contributions from internationally recognized experts from the Americas, Asia, and the EU, this authoritative, self-contained reference includes best practices and specification data spanning the gamut of simulation tools available internationally that can be used to speed up the certification of aircraft and make them safer to fly into known icing. The collection features nine sections concentrating on aircraft, rotorcraft, jet engines, UAVs; ice protection systems, including hot-air, electrothermal, and others; sensors and probes, CFD in the aid of testing, flight simulators, and certification process acceleration methods. Incorporating perspectives from academia, commercial, government R&D, the book is ideal for a range of engineers and scientists concerned with in-flight icing applications... ..
出版日期Living reference work 20200th edition
关键词In-Flight Icing; Computational Fluid Dynamics; CFD; Numerical Simulation; Icing Science; Aircraft; Jet eng
doihttps://doi.org/10.1007/978-3-030-64725-4
isbn_ebook978-3-030-64725-4
The information of publication is updating

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发表于 2025-3-21 23:52:42 | 显示全部楼层
Numerical Simulation of Iced Swept Wing Aerodynamics with RANS, DES, and IDDES,where the coefficient became non-linear, e.g., the pitching moment break in the experimental data. In particular, DES and IDDES did not quantitatively capture the spanwise component of the flow over the stalled portions of the swept wing nor did they properly predict the pressure distribution along
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Numerical Simulation of Supercooled Droplets Freezing During In-Flight Icing via a Hybrid Numericale one-dimensional suspended droplet. The two approaches may be applied independently or in combination, for instance, in simplifying the multi-dimensional local models into a lumped-differential formulation through CIEA, which is then solved by the hybrid GITT methodology. The model reduction and si
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Numerical Simulation of Coupled Heat and Mass Transfer for Airfoil Ice Protection Systems,-state regime. In addition to the effects of phase change by evaporation, freezing, and melting, the code considers the impact of the streamwise temperature gradient, water hydrodynamics, and laminar-turbulent transition. Correlations predict both the onset and length of the laminar-turbulent transi
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