Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書 pdf 下載 txt下載 epub 下載 mobi 下載 2024

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Verhaagen, N. G. 作者

譯者

出版日期

516 頁數

$ 326.57 價格

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9781402093326 圖書編碼

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發表於2024-09-20

Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書 epub 下載 mobi 下載 pdf 下載 txt 下載 2024

Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書 epub 下載 pdf 下載 mobi 下載 txt 下載 2024

Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書 pdf 下載 txt下載 epub 下載 mobi 下載 2024

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Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書 pdf 下載 txt下載 epub 下載 mobi 在線電子書下載

Vortex Flow Behavior Over Slender Delta Wing Configurations 在線電子書圖書描述

The book discusses the behavior of vortices over sharp and highly swept wing configurations used for current and future military aircraft. Special attention is paid to the effects of critical flow phenomenon such as vortex breakdown occuring at high angles of attack or high angular rates. The wind tunnel experiments conducted on delta-wing configurations in wind tunnels in Canada, Europe, Russia and the United States are given in eight chapters. The experiments provide an extended data base that gives insight into the effects of the angle of attack, angular rate, Reynolds number and Mach number on the behavior of vortices over several slender delta wings in stationary and instationary flights. A critical assessment is given in a separated chapter of the available experimental data bases and out of these data, one and the same data set is selected for the validation and verification of analytical and numerical solutions.Comprehansive computational results are given in another ten chapters. Steady-state and time-accurate solutions for the steady and unsteady flow over the selected delta-wing configuration are discussed. These solutions are generated using structured and unstructured grid methods.The analytical solutions for the flow over a delta wing are discussed and compared with experimental data in three more chapters.In the final chapter a validation and verification of the analytical and CFD solutions is given.

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