已入深夜,您辛苦了!由于当前在线用户较少,发布求助请尽量完整的填写文献信息,科研通机器人24小时在线,伴您度过漫漫科研夜!祝你早点完成任务,早点休息,好梦!

Analysis of Averaging Methods for Nonuniform Total Pressure Fields

加权 马赫数 空气动力学 涡轮机械 航程(航空) 机械 数学 平面(几何) 喷嘴 流量(数学) 物理 工程类 几何学 声学 机械工程 航空航天工程
作者
Daniel Burdett,Thomas Povey
出处
期刊:Journal of turbomachinery [ASME International]
卷期号:144 (5) 被引量:4
标识
DOI:10.1115/1.4053020
摘要

Abstract A common objective in the analysis of turbomachinery components (nozzle guide vanes (NGVs) or rotor blades, for example) is to calculate performance parameters, such as total pressure or kinetic energy (KE) loss coefficients, from measurements in a nonuniform flow-field. These performance parameters can be represented in a range of ways. For example, line-averages used to compare performance between different radial sections of a 3D component; plane-averages used to assess flow (perhaps loss coefficient) development between different axial planes; and fully mixed-out values used to determine the total loss associated with a component. In the literature, the weighting method used for line- and plane-averaging (e.g., area, volume flow, mass flow, or entropy-flux) is sometimes regarded as an unimportant issue. Indeed, many authors neglect to even state which weighting method was used in their work. In certain low-speed test cases, or where measurements are made a long distance from the component, the nonuniformity in the flow will be relatively small and the practical difference between different weighting methods may be negligible. However, in high-speed applications or for measurements close to a component trailing edge, this becomes increasingly unlikely. In this paper, we compare a range of methods for calculating aerodynamic performance parameters—for example, the kinetic energy loss coefficient—including plane-average methods with different weighting schemes and several mixed-out methods. We analyze the sensitivities of the different methods to the axial location of the measurement plane, the radial averaging range, and the exit Mach number. We use high-fidelity experimental data taken in several axial planes downstream of a cascade of engine parts: high-pressure (HP) turbine NGVs operating at transonic Mach number. The experimental data are complemented by computational fluid dynamics (CFD). We discuss the underlying physical mechanisms which give rise to the observed sensitivities. The objective is to provide guidance on the accuracy of each method in a relevant, practical application.

科研通智能强力驱动
Strongly Powered by AbleSci AI
更新
大幅提高文件上传限制,最高150M (2024-4-1)

科研通是完全免费的文献互助平台,具备全网最快的应助速度,最高的求助完成率。 对每一个文献求助,科研通都将尽心尽力,给求助人一个满意的交代。
实时播报
刚刚
怡然的一凤完成签到 ,获得积分10
4秒前
5秒前
小屁孩应助加菲丰丰采纳,获得20
5秒前
7秒前
7秒前
iwaking完成签到,获得积分10
7秒前
不安夜雪完成签到 ,获得积分10
8秒前
科研通AI2S应助zf2023采纳,获得10
10秒前
漠北发布了新的文献求助10
10秒前
阿泽发布了新的文献求助10
10秒前
子车谷波发布了新的文献求助10
11秒前
11秒前
科研通AI2S应助程风破浪采纳,获得10
12秒前
婉约清扬完成签到 ,获得积分10
12秒前
风趣的惜天完成签到 ,获得积分10
13秒前
今后应助上岸采纳,获得10
18秒前
大模型应助yeluoyezhi采纳,获得10
18秒前
低调000完成签到,获得积分10
20秒前
22秒前
赘婿应助雪楼风铃采纳,获得30
23秒前
蜂蜜柚子完成签到 ,获得积分10
26秒前
28秒前
小蘑菇应助科研通管家采纳,获得10
31秒前
斯文败类应助科研通管家采纳,获得10
31秒前
星辰大海应助科研通管家采纳,获得30
31秒前
小蘑菇应助科研通管家采纳,获得10
31秒前
32秒前
33秒前
李爱国应助一只小羊采纳,获得10
33秒前
33秒前
无言已对发布了新的文献求助10
33秒前
小蘑菇应助prtrichor599采纳,获得10
35秒前
36秒前
37秒前
我是老大应助zjh采纳,获得10
38秒前
yeluoyezhi发布了新的文献求助10
39秒前
柚子发布了新的文献求助10
41秒前
友好醉波完成签到 ,获得积分10
41秒前
小二郎应助勺子采纳,获得10
43秒前
高分求助中
Shape Determination of Large Sedimental Rock Fragments 2000
Sustainability in Tides Chemistry 2000
Rechtsphilosophie 1000
Bayesian Models of Cognition:Reverse Engineering the Mind 888
A Dissection Guide & Atlas to the Rabbit 600
Very-high-order BVD Schemes Using β-variable THINC Method 568
Mantiden: Faszinierende Lauerjäger Faszinierende Lauerjäger 500
热门求助领域 (近24小时)
化学 医学 生物 材料科学 工程类 有机化学 生物化学 物理 内科学 纳米技术 计算机科学 化学工程 复合材料 基因 遗传学 催化作用 物理化学 免疫学 量子力学 细胞生物学
热门帖子
关注 科研通微信公众号,转发送积分 3129906
求助须知:如何正确求助?哪些是违规求助? 2780653
关于积分的说明 7749626
捐赠科研通 2435992
什么是DOI,文献DOI怎么找? 1294442
科研通“疑难数据库(出版商)”最低求助积分说明 623673
版权声明 600570