Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(meanline). Showing records 1 – 5 of 5 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters

1. Mikaillian, Navid. Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations.

Degree: Heat and Power Technology, 2012, KTH

  This thesis is a collaboration between Siemens Industrial Turbomachinery(SIT) and Royal Institute of Technology(KTH). It is aimed to study and compare the outputs of… (more)

Subjects/Keywords: Gas Turbine; Meanline; Throughflow

…programs used at SIT are MAC1 and BETA2. The former is a 1D meanline code that simplifies the… …before e.g. by use of another Siemens code, AXIAL, which is a meanline code and the results… …computationally. In computation phase, the results from the meanline and the throughflow codes are… …modeler, meanline and throughflow solvers. The main structure of solvers input file immediately… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Mikaillian, N. (2012). Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104578

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Mikaillian, Navid. “Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations.” 2012. Thesis, KTH. Accessed April 04, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104578.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Mikaillian, Navid. “Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations.” 2012. Web. 04 Apr 2020.

Vancouver:

Mikaillian N. Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations. [Internet] [Thesis]. KTH; 2012. [cited 2020 Apr 04]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104578.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mikaillian N. Test Turbine Measurements and Comparison with Meanline and Throughflow Calculations. [Thesis]. KTH; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104578

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

2. Muppana, Sai. Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 Centrifugal compressors are favorable because they can generate high pressure ratio due to large change in radius from inlet to exit of compressor. This increase… (more)

Subjects/Keywords: Aerospace Materials; Centrifugal compressor; multi-rotor; CFD; blade design; meanline analysis; stall

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Muppana, S. (2018). Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1553517075653458

Chicago Manual of Style (16th Edition):

Muppana, Sai. “Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor.” 2018. Masters Thesis, University of Cincinnati. Accessed April 04, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1553517075653458.

MLA Handbook (7th Edition):

Muppana, Sai. “Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor.” 2018. Web. 04 Apr 2020.

Vancouver:

Muppana S. Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2020 Apr 04]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1553517075653458.

Council of Science Editors:

Muppana S. Multi-fidelity Design and Analysis of Single Hub Multi-rotor High Pressure Centrifugal Compressor. [Masters Thesis]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1553517075653458


North-West University

3. Swift, William James. Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift .

Degree: 2003, North-West University

 The need was identified to develop an analytical performance prediction code for subsonic multistage axial compressors that can be included in network analysis software. It… (more)

Subjects/Keywords: Loss; Axial; Compressor; Modelling; Performance; Prediction; Subsonic; Meanline; Mechanisms

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Swift, W. J. (2003). Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift . (Thesis). North-West University. Retrieved from http://hdl.handle.net/10394/431

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Swift, William James. “Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift .” 2003. Thesis, North-West University. Accessed April 04, 2020. http://hdl.handle.net/10394/431.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Swift, William James. “Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift .” 2003. Web. 04 Apr 2020.

Vancouver:

Swift WJ. Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift . [Internet] [Thesis]. North-West University; 2003. [cited 2020 Apr 04]. Available from: http://hdl.handle.net/10394/431.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Swift WJ. Modelling of losses in multi-stage axial compressors with subsonic conditions / William James Swift . [Thesis]. North-West University; 2003. Available from: http://hdl.handle.net/10394/431

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Brigham Young University

4. Pelton, Robert John. One-Dimensional Radial Flow Turbomachinery Performance Modeling.

Degree: MS, 2007, Brigham Young University

 The Two-Element In Series (TEIS) and Two-Zone models have been used successfully for over twenty years to model test data for radial flow compressors and… (more)

Subjects/Keywords: TEIS; Two-Zone; turbomachinery; one-dimensional; meanline; compressor; modeling; impeller; Mechanical Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Pelton, R. J. (2007). One-Dimensional Radial Flow Turbomachinery Performance Modeling. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2252&context=etd

Chicago Manual of Style (16th Edition):

Pelton, Robert John. “One-Dimensional Radial Flow Turbomachinery Performance Modeling.” 2007. Masters Thesis, Brigham Young University. Accessed April 04, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2252&context=etd.

MLA Handbook (7th Edition):

Pelton, Robert John. “One-Dimensional Radial Flow Turbomachinery Performance Modeling.” 2007. Web. 04 Apr 2020.

Vancouver:

Pelton RJ. One-Dimensional Radial Flow Turbomachinery Performance Modeling. [Internet] [Masters thesis]. Brigham Young University; 2007. [cited 2020 Apr 04]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2252&context=etd.

Council of Science Editors:

Pelton RJ. One-Dimensional Radial Flow Turbomachinery Performance Modeling. [Masters Thesis]. Brigham Young University; 2007. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2252&context=etd


Delft University of Technology

5. Javed, A. Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor.

Degree: 2014, Delft University of Technology

Subjects/Keywords: turbomachinery; centrifugal compressor; Computational Fluid Dynamics; 1D Meanline Modeling; Robust Design Optimization; uncertainty quantification; manufacturing; turbochargers

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Javed, A. (2014). Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2

Chicago Manual of Style (16th Edition):

Javed, A. “Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor.” 2014. Doctoral Dissertation, Delft University of Technology. Accessed April 04, 2020. http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2.

MLA Handbook (7th Edition):

Javed, A. “Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor.” 2014. Web. 04 Apr 2020.

Vancouver:

Javed A. Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor. [Internet] [Doctoral dissertation]. Delft University of Technology; 2014. [cited 2020 Apr 04]. Available from: http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2.

Council of Science Editors:

Javed A. Developing Generic Design Expertise for Gas Turbine Engines: Robust Design of a Micro Centrifugal Compressor. [Doctoral Dissertation]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; urn:NBN:nl:ui:24-uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2 ; http://resolver.tudelft.nl/uuid:fe3f5b92-bae9-4450-ad52-e8be2145c5e2

.