ESDU 79009-1979由ESDU - Engineering Sciences Data Unit 发布于 1979-10-01,并于 2004-05-14 实施。
。
ESDU 79009 presents the theoretical basis for three methods available in the literature. All are restricted to isentropic flow and one is further restricted to flows without shocks and thus at transonic speeds to only just-supercritical flows. Of the remaining two@ one@ strictly@ is limited to freestream Mach numbers close to unity but has been adapted to yield useful solutions over a wider range of Mach numbers. The way in which the three techniques are used is described@ recommendations are made on the values to be assigned to certain variable parameters within the programs@ the range of applicability is indicated@ and evaluations made of the programs are discussed. Example solutions of pressure distributions obtained using the programs for specific cases are given graphically and provide valuable test cases for those using the programs for the first time.
对此方程组的求解支持您构建半导体器件的电压-电流特征。半导体方程高度非线性,需要特殊的数值方法来求解。我们全新的半导体模块正如我们最近所宣布的,COMSOL 平台新近增加了专业的半导体模拟产品,即半导体模块,它可以帮助用户从基础物理水平层面对半导体器件进行详细分析。...
现在对叶片的研究广泛应用了CFD ( computational fluid dynamics)技术,即计算流体动力学技术,其原理是将空间域上连续的物理量的场用一系列有限个离散点上的变量值的集合来代替,通过一定的原则和方式 建立起关于这些离散点上场变量之间关系的代数方程组,然后求解代数方程组获得场变量的近似值,CFD可以看作是在流体基本方程(质量守恒方程、动量守恒方 程和能量守恒方程)控制下对流体的数值模拟...
因此如何设计发动机使其能够兼顾超音速客机亚音速和超音速两种飞行状态,也是一个技术难点。 或许超音速客机“再现”的难题不止于此。中国民用航空飞行学院教师岳源谈到,首先超音速客机外载荷更大,对飞机材料和结构的要求更高,特别是对机翼翼根的强度、刚度要求会更高。其次,现在客机主要使用超临界翼型,主要用在跨音速阶段的飞行,不适用于超音速飞行。适用于超音速飞行多是战斗机,这类飞机相比客机展弦比要小得多。...
研究发现,新型翼型流道的火积耗散数和欧拉数比传统翼型流道小,具有更好的热工水力特性。基于实验和数值模拟结果,获得了新型翼型流道内含湿烟气流动传热关联式(见图1)。...
Copyright ©2007-2022 ANTPEDIA, All Rights Reserved
京ICP备07018254号 京公网安备1101085018 电信与信息服务业务经营许可证:京ICP证110310号