The purpose of this work is to study the aerodynamic performance of a tandem C4 base-profile compressor blade using numerical tools. In this paper, the flow along the tandem blade is studied for various relative blade positions. In all the studied cases, the front blade is fixed and the position of the rear blade is varied as a function of the axial and tangential displacements. A computer code was developed in "Visual Basic" using linear strength vortex-panel method to predict the aerodynamic performance of the tandem blade.
| Published in |
American Journal of Aerospace Engineering (Volume 2, Issue 1-1)
This article belongs to the Special Issue Hands-on Learning Technique for Multidisciplinary Engineering Education |
| DOI | 10.11648/j.ajae.s.2015020101.17 |
| Page(s) | 74-92 |
| Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
| Copyright |
Copyright © The Author(s), 2024. Published by Science Publishing Group |
Tandem Blades, Linear Strength Vortex Panel Method, Rotor, Stator, Axial-Compressor
| [1] | A. J. Wennerstrom, "Low aspect ratio axial flow compressors: why and what it means," ASME Journal of Turbomachinery, Vol. 111, pp. 357-365, 1989. |
| [2] | A. K. Saha, and B. Roy, "Experimental analysis of controlled diffusion compressor cascades with single and tandem airfoils," ASME paper number 95-CTP-41, 1995. |
| [3] | A. K. Saha, and B. Roy, "Experimental investigations on tandem compressor cascade performance at low speeds," Experimental Thermal and Fluid Science, Vol. 14, pp. 263-276, 1997. |
| [4] | E. Sheets, "Multiple row blades for blowers," ASME paper number 88-GT-124, 1988. |
| [5] | A. Weber, and W. Steinert, "Design, Optimization, and Analysis of a High-Turning Transonic Tandem Compressor Cascade," ASME paper number 97-GT-412, 1997. |
| [6] | General Electric Co. Manuals, Al-shabab Power Plant (1000 MW-simple gas turbine plant), Ismailia, Egypt. |
| [7] | K. Bammert, and H. Beelte, "Investigations of an axial flow compressor with tandem cascades," ASME Journal of Engineering Power, pp. 971-977, October 1980. |
| [8] | K. Bammert, and R. Staude, "Optimization for rotor blades of tandem design for axial flow compressors," ASME Journal of Engineering for Power, pp. 369-375, April 1980. |
| [9] | J. McGlumphy, 2-D computational studies of subsonic axial rotors incorporating dual airfoils, UTSR Project Report for summer 2005. |
| [10] | J. McGlumphy, W.-F. Ng, S. R. Wellborn, and S. Kempf, "Numerical investigation of tandem airfoils for subsonic axial- flow compressor blades," Journal of Turbomachinery, Vol. 131, pp. 1-8, April 2009. |
| [11] | J. McGlumphy, W.-F. Ng, S. R. Wellborn, and S. Kempf, "3D numerical investigation of tandem airfoils for a core compressor rotor," Journal of Turbomachinery, Vol. 132, pp. 1-9, July 2010. |
| [12] | G. A. Canon, Numerical investigation of the flow in tandem compressor cascade, Diploma Thesis, Vienna University of Technology, Austria, 2004. |
| [13] | J. Katz, and A. Plotkin, Low-Speed Aerodynamics, 2nd ed., Cambridge University Press, 2001. |
| [14] | C. A. Cox, Two Element Linear Strength Vortex Panel Method, Senior Project, Faculty of the Aerospace Engineering, California Polytechnic State University, San Luis, USA, March 2011. |
APA Style
Atef Mohamed Alm-Eldien, Ahmed Farouk Abdel Gawad, Gamal Hafaz, Mohamed Gaber Abd El Kreim. (2014). Performance Evaluation of the Tandem C4 Blades for Axial-Flow Compressors. American Journal of Aerospace Engineering, 2(1-1), 74-92. https://doi.org/10.11648/j.ajae.s.2015020101.17
ACS Style
Atef Mohamed Alm-Eldien; Ahmed Farouk Abdel Gawad; Gamal Hafaz; Mohamed Gaber Abd El Kreim. Performance Evaluation of the Tandem C4 Blades for Axial-Flow Compressors. Am. J. Aerosp. Eng. 2014, 2(1-1), 74-92. doi: 10.11648/j.ajae.s.2015020101.17
AMA Style
Atef Mohamed Alm-Eldien, Ahmed Farouk Abdel Gawad, Gamal Hafaz, Mohamed Gaber Abd El Kreim. Performance Evaluation of the Tandem C4 Blades for Axial-Flow Compressors. Am J Aerosp Eng. 2014;2(1-1):74-92. doi: 10.11648/j.ajae.s.2015020101.17
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Download@article{10.11648/j.ajae.s.2015020101.17,
author = {Atef Mohamed Alm-Eldien and Ahmed Farouk Abdel Gawad and Gamal Hafaz and Mohamed Gaber Abd El Kreim},
title = {Performance Evaluation of the Tandem C4 Blades for Axial-Flow Compressors},
journal = {American Journal of Aerospace Engineering},
volume = {2},
number = {1-1},
pages = {74-92},
doi = {10.11648/j.ajae.s.2015020101.17},
url = {https://doi.org/10.11648/j.ajae.s.2015020101.17},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.s.2015020101.17},
abstract = {The purpose of this work is to study the aerodynamic performance of a tandem C4 base-profile compressor blade using numerical tools. In this paper, the flow along the tandem blade is studied for various relative blade positions. In all the studied cases, the front blade is fixed and the position of the rear blade is varied as a function of the axial and tangential displacements. A computer code was developed in "Visual Basic" using linear strength vortex-panel method to predict the aerodynamic performance of the tandem blade.},
year = {2014}
}
TY - JOUR T1 - Performance Evaluation of the Tandem C4 Blades for Axial-Flow Compressors AU - Atef Mohamed Alm-Eldien AU - Ahmed Farouk Abdel Gawad AU - Gamal Hafaz AU - Mohamed Gaber Abd El Kreim Y1 - 2014/10/17 PY - 2014 N1 - https://doi.org/10.11648/j.ajae.s.2015020101.17 DO - 10.11648/j.ajae.s.2015020101.17 T2 - American Journal of Aerospace Engineering JF - American Journal of Aerospace Engineering JO - American Journal of Aerospace Engineering SP - 74 EP - 92 PB - Science Publishing Group SN - 2376-4821 UR - https://doi.org/10.11648/j.ajae.s.2015020101.17 AB - The purpose of this work is to study the aerodynamic performance of a tandem C4 base-profile compressor blade using numerical tools. In this paper, the flow along the tandem blade is studied for various relative blade positions. In all the studied cases, the front blade is fixed and the position of the rear blade is varied as a function of the axial and tangential displacements. A computer code was developed in "Visual Basic" using linear strength vortex-panel method to predict the aerodynamic performance of the tandem blade. VL - 2 IS - 1-1 ER -
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