東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Design and performance analysis of g...

Tan, Xu.

FindBook

Google Book

Amazon

博客來

Design and performance analysis of gas and liquid radial turbines.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Design and performance analysis of gas and liquid radial turbines./
作者:	Tan, Xu.
面頁冊數:	177 p.
附註:	Source: Dissertation Abstracts International, Volume: 78-05(E), Section: B.
Contained By:	Dissertation Abstracts International78-05B(E).
標題:	Mechanical engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10247894
ISBN:	9781369433128

Design and performance analysis of gas and liquid radial turbines.
Tan, Xu.

Design and performance analysis of gas and liquid radial turbines. - 177 p.

Source: Dissertation Abstracts International, Volume: 78-05(E), Section: B.

Thesis (Ph.D.)--Michigan State University, 2016.

In the first part of the research, pumps running in reverse as turbines are studied. This work uses experimental data of wide range of pumps representing the centrifugal pumps' configurations in terms of specific speed. Based on specific speed and specific diameter an accurate correlation is developed to predict the performances at best efficiency point of the centrifugal pump in its turbine mode operation. The proposed prediction method yields very good results to date compared to previous such attempts. The present method is compared to nine previous methods found in the literature. The comparison results show that the method proposed in this paper is the most accurate. The proposed method can be further complemented and supplemented by more future tests to increase its accuracy. The proposed method is meaningful because it is based both specific speed and specific diameter.

ISBN: 9781369433128Subjects--Topical Terms:

649730
Mechanical engineering.

Design and performance analysis of gas and liquid radial turbines.
LDR:02649nmm a2200301 4500 001 2115318
005 20170228070047.5
008 180830s2016 ||||||||||||||||| ||eng d
020 $a 9781369433128
035 $a (MiAaPQ)AAI10247894
035 $a AAI10247894
040 $a MiAaPQ $c MiAaPQ
100 1 $a Tan, Xu. $3 3276962
245 1 0 $a Design and performance analysis of gas and liquid radial turbines.
300 $a 177 p.
500 $a Source: Dissertation Abstracts International, Volume: 78-05(E), Section: B.
500 $a Adviser: Abraham Engeda.
502 $a Thesis (Ph.D.)--Michigan State University, 2016.
520 $a In the first part of the research, pumps running in reverse as turbines are studied. This work uses experimental data of wide range of pumps representing the centrifugal pumps' configurations in terms of specific speed. Based on specific speed and specific diameter an accurate correlation is developed to predict the performances at best efficiency point of the centrifugal pump in its turbine mode operation. The proposed prediction method yields very good results to date compared to previous such attempts. The present method is compared to nine previous methods found in the literature. The comparison results show that the method proposed in this paper is the most accurate. The proposed method can be further complemented and supplemented by more future tests to increase its accuracy. The proposed method is meaningful because it is based both specific speed and specific diameter.
520 $a The second part of the research is focused on the design and analysis of the radial gas turbine. The specification of the turbine is obtained from the solar biogas hybrid system. The system is theoretically analyzed and constructed based on the purchased compressor. Theoretical analysis results in a specification of 100lb/min, 900ºC inlet total temperature and 1.575atm inlet total pressure.
520 $a 1-D and 3-D geometry of the rotor is generated based on Aungier's method. 1-D loss model analysis and 3-D CFD simulations are performed to examine the performances of the rotor. The total-to-total efficiency of the rotor is more than 90%. With the help of CFD analysis, modifications on the preliminary design obtained optimized aerodynamic performances. At last, the theoretical performance analysis on the hybrid system is performed with the designed turbine.
590 $a School code: 0128.
650 4 $a Mechanical engineering. $3 649730
650 4 $a Aerospace engineering. $3 1002622
690 $a 0548
690 $a 0538
710 2 $a Michigan State University. $b Mechanical Engineering. $3 2102783
773 0 $t Dissertation Abstracts International $g 78-05B(E).
790 $a 0128
791 $a Ph.D.
792 $a 2016
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10247894