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Titlebook: A Theory of Supercritical Wing Sections, with Computer Programs and Examples; With Computer Progra Frances Bauer,Paul Garabedian,David Korn

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发表于 2025-3-21 18:11:46 | 显示全部楼层 |阅读模式
期刊全称A Theory of Supercritical Wing Sections, with Computer Programs and Examples
期刊简称With Computer Progra
影响因子2023Frances Bauer,Paul Garabedian,David Korn
视频video
学科分类Lecture Notes in Economics and Mathematical Systems
图书封面Titlebook: A Theory of Supercritical Wing Sections, with Computer Programs and Examples; With Computer Progra Frances Bauer,Paul Garabedian,David Korn
影响因子At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati­ cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part.
Pindex Book 1972
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发表于 2025-3-21 21:29:32 | 显示全部楼层
Examples,von Maschinen und Anlagen sind häufig Resultate hydraulischer und pneumatischer Antriebs- und Steuerungstechnik. Bei linearen wie auch rotatorischen Bewegungen, gleichmäßigen Huboder Senkbewegungen, Beschleunigungsforderungen, Leistungsübertragungen oder dem Bedarf Positionen anzufahren und zu halte
发表于 2025-3-22 00:28:57 | 显示全部楼层
发表于 2025-3-22 08:36:24 | 显示全部楼层
发表于 2025-3-22 09:58:01 | 显示全部楼层
Examples,Maschine oder ein Flugzeug bewegt sich ohne sie – nur ist es uns meistens nicht bewusst. Die Hydraulikund Pneumatikhersteller sind Zulieferer für die gesamte Industrie. Zu ihren Abnehmerbranchen zählen z. B. die Automobilindustrie, die Baumaschinen- und Landmaschinenindustrie, die Fördertechnik, die
发表于 2025-3-22 16:41:40 | 显示全部楼层
发表于 2025-3-22 18:10:29 | 显示全部楼层
Book 1972 we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati­ cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part.
发表于 2025-3-23 00:08:25 | 显示全部楼层
发表于 2025-3-23 04:35:07 | 显示全部楼层
Dying as liminality in the making,ying this manual it should be possible to learn how to operate the design and analysis programs even with only a limited understanding of the mathematical content. We intend to make the basic method available to those interested in designing transonic airfoils but unwilling to spend the time require
发表于 2025-3-23 08:21:25 | 显示全部楼层
https://doi.org/10.1057/978-1-137-53849-9numbers of test runs of the program to produce, with the earliest case requiring hundreds of trials, but the later ones needing less as we gained experience. All models were designed to have a maximum thickness-chord ratio T/C for given free stream Mach number M. and lift coefficient C., subject to
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