A gas turbine, also called a combustion turbine, is a type of internal combustion engine obtains its power by utilizing the energy of burnt gases and the air which is at high temperature and pressure by expanding through the several rings of fixed and moving blades mounted over a disc. The major function of the turbine is to extract energy from the hot gas flow to drive the compressor and the accessory gearbox. Gas turbine discs work mostly at high temperature gradients and are subjected to high rotational velocity. High speed results in large centrifugal forces in discs and simultaneous high temperature results in thermal stress. The stress which greatly influence the design of turbine disc is the thermal stress. Thus a model of H.P turbine is created using CATIA V5 and the exported to ANSYS 16.0 to perform transient thermal analysis. The thermal analysis performed with three different materials i.e. SUPERALLOY A286, INCONEL 718, and UDIMET 720. The comparison of all material will result in better use of turbine disc material at different stages of combustion.
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IJRTI — journal style
"Design and analysis of Aero Turbine disc by fea: a review", IJRTI - International Journal for Research Trends and Innovation (www.ijrti.org), ISSN:2456-3315, Vol.3, Issue 6, page no.206 - 208, June-2018, Available :https://ijrti.org/papers/IJRTI1806039.pdf
APA — 7th edition
DADLANI, M., & JOSHI, U. K. (2018). Design and analysis of Aero Turbine disc by fea: a review. International Journal for Research Trends and Innovation, 3(6), 206 - 208. https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039
MLA — 9th edition
DADLANI, MOHIT, and U.K JOSHI. "Design and analysis of Aero Turbine disc by fea: a review." International Journal for Research Trends and Innovation, vol. 3, no. 6, 2018, pp. 206 - 208, https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039.
Chicago — 17th, bibliography
DADLANI, MOHIT, and U.K JOSHI. "Design and analysis of Aero Turbine disc by fea: a review." International Journal for Research Trends and Innovation 3, no. 6 (2018): 206 - 208. https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039.
Harvard — author–date
DADLANI, M. and JOSHI, U.K. (2018) 'Design and analysis of Aero Turbine disc by fea: a review', International Journal for Research Trends and Innovation, 3(6), pp. 206 - 208. Available at: https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039
IEEE — numbered reference
M. DADLANI and U. K. JOSHI, "Design and analysis of Aero Turbine disc by fea: a review," IJRTI, vol. 3, no. 6, pp. 206 - 208, Jun. 2018.
Vancouver — biomedical
DADLANI M, JOSHI UK. Design and analysis of Aero Turbine disc by fea: a review. IJRTI. 2018 Jun;3(6):206 - 208.
AMA — 11th edition
DADLANI M, JOSHI UK. Design and analysis of Aero Turbine disc by fea: a review. IJRTI. 2018;3(6):206 - 208. Accessed at https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039
BibTeX — Zotero, Mendeley, LaTeX
@article{IJRTI1806039,
author = {MOHIT DADLANI and U.K JOSHI},
title = {Design and analysis of Aero Turbine disc by fea: a review},
journal = {International Journal for Research Trends and Innovation},
volume = {3},
number = {6},
pages = {206 - 208},
year = {2018},
month = {June},
issn = {2456-3315},
url = {https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039}
}
RIS — EndNote, RefWorks
TY - JOUR
AU - DADLANI, MOHIT
AU - JOSHI, U.K
TI - Design and analysis of Aero Turbine disc by fea: a review
T2 - International Journal for Research Trends and Innovation
JA - IJRTI
VL - 3
IS - 6
PY - 2018
SN - 2456-3315
UR - https://ijrti.org/viewpaperforall.php?paper=IJRTI1806039
SP - 206
EP - 208
ER -
International Journal for Research Trends and InnovationPublished by IJRTI (JW Publication)
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Acknowledgements
The authors would like to thank the reviewers and the editorial board of International Journal for Research Trends and Innovation for their careful reading and constructive comments, and all colleagues who supported the preparation of this manuscript.