Development and Validation of a Computational Code for Wet Compression Simulation of Gas Turbines

Author:

Bagnoli M.1,Bianchi M.1,Melino F.1,Spina P. R.2

Affiliation:

1. DIEM, University of Bologna, Viale del Risorgimento 2, 40136 Bologna, Italy

2. ENDIF, University of Ferrara, Via Saragat, 44100 Ferrara, Italy

Abstract

In this paper, a calculation code, developed in house by the authors, able to evaluate the performance of a gas turbine with all possible fogging strategies (high pressure fogging, overspray, and interstage injection) is presented and discussed. The code has a flexible structure and can be applied to evaluate the performance of every commercial gas turbine model. The aim of the calculation code is to overcome the limits of the most widespread commercial software, especially with regard to the two phase flow compression process simulation. The calculation code was validated on results available in the literature showing a good agreement with experimental and theoretical results.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference23 articles.

1. Tawney, R., Pearson, C., and Brown, M., 2001, “Options to Maximize Power Output for Merchant Plants in Combined Cycle Applications,” ASME Paper No. 2001-GT-0409.

2. Bianchi, M., Melino, F., Peretto, A., Bhargava, R. K., Chaker, M. C., Ingistov, S., and Meher-Homji, C. B., 2005, “Gas Turbine Fogging Technology: A State of the Art Review, Part I: Inlet and Evaporative Fogging—Analytical and Experimental Aspects,” ASME Paper No. GT2005-68336.

3. Value of Wet Compression in Gas-Turbine Cycles;Kleinschmidt;Mech. Eng. (Am. Soc. Mech. Eng.)

4. Wilcox, E. C., and Trout, A. M., 1951, “Analysis of Thrust Augmentation of Turbojet Engines by Water Injection at Compressor Inlet Including Charts for Calculating Compression Process with Water Injection,” NACA Report No. 1006.

5. Aerodynamic and Thermodynamic Effects of Coolant Injection on Axial Compressors;Hill;Aeronaut. Q.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3