Turbine blade (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Turbine blade" in English language version.

refsWebsite

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5doi.org

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3sciencedirect.com

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2patents.google.com

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1turboaerodesign.com

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1gereports.com

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1specialmetals.com

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1archive.today

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americanscientist.org

Langston, Lee S. (6 February 2017). "Each Blade a Single Crystal". www.americanscientist.org. Retrieved 25 November 2018.

archive.today

"Products." Archived 8 December 2012 at archive.today Special Metals. Retrieved: 5 March 2011.

books.google.com

Yahya, S M (2011). Turbines Compressors and Fans. New delhi: Tata McGraw-Hill Education, 2010. pp. 430–433. ISBN 9780070707023.

doe.gov

netl.doe.gov

Lesley M. Wright, Je-Chin Han. "Enhanced Internal Cooling of Turbine Blades and Vanes". 4.2.2.2 Enhanced Internal Coolingof Turbine Blades and Vanes. Retrieved 27 May 2013.

doi.org

Acharya, Sumanta; Kanani, Yousef (2017-01-01), Sparrow, Ephraim M.; Abraham, John P.; Gorman, John M. (eds.), "Chapter Three - Advances in Film Cooling Heat Transfer", Advances in Heat Transfer, vol. 49, Elsevier, pp. 91–156, doi:10.1016/bs.aiht.2017.10.001, retrieved 2019-08-30
Goldstein, Richard J. (1971-01-01), "Film Cooling", in Irvine, Thomas F.; Hartnett, James P. (eds.), Advances in Heat Transfer Volume 7, vol. 7, Elsevier, pp. 321–379, doi:10.1016/s0065-2717(08)70020-0, ISBN 9780120200078, retrieved 2019-08-30
Bogard, D. G.; Thole, K. A. (2006-03-01). "Gas Turbine Film Cooling" (PDF). Journal of Propulsion and Power. 22 (2): 249–270. doi:10.2514/1.18034. S2CID 54063370. Archived from the original (PDF) on 2019-03-07.
Bhagi LK, Rastogi V, Gupta P (2017). "Study of corrosive fatigue and life enhancement of low pressure steam turbine blade using friction dampers". Journal of Mechanical Science and Technology. 31: 17–27. doi:10.1007/s12206-016-1203-5. S2CID 115023151.
Halbig, Jaskowiak, Kiser, Zhu (June 2013). "Evaluation of Ceramic Matrix Composite Technology for Aircraft Turbine Engine Applications" (PDF). 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. doi:10.2514/6.2013-539. hdl:2060/20130010774. ISBN 978-1-62410-181-6.{{cite journal}}: CS1 maint: multiple names: authors list (link)

geaviation.com

"GE Successfully Tests World's First Rotating Ceramic Matrix Composite Material for Next-Gen Combat Engine | Press Release | GE Aviation". www.geaviation.com. Retrieved 2 November 2015.

gereports.com

"Ceramic Matrix Composites Allow GE Jet Engines to Fly Longer – GE Reports". GE Reports. Retrieved 2 November 2015.

handle.net

hdl.handle.net

Halbig, Jaskowiak, Kiser, Zhu (June 2013). "Evaluation of Ceramic Matrix Composite Technology for Aircraft Turbine Engine Applications" (PDF). 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. doi:10.2514/6.2013-539. hdl:2060/20130010774. ISBN 978-1-62410-181-6.{{cite journal}}: CS1 maint: multiple names: authors list (link)

ihi.co.jp

Takeshi, Takashi, Kuniyuki, Ken-ichi, Masato. "Development of CMC Turbine Parts for Aero Engines" (PDF).{{cite web}}: CS1 maint: multiple names: authors list (link)

machinedesign.com

Langston, Lee S. (16 March 2018). "Single-Crystal Turbine Blades Earn ASME Milestone Status". www.machinedesign.com. Retrieved 25 November 2018.

nasa.gov

ntrs.nasa.gov

Halbig, Jaskowiak, Kiser, Zhu (June 2013). "Evaluation of Ceramic Matrix Composite Technology for Aircraft Turbine Engine Applications" (PDF). 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. doi:10.2514/6.2013-539. hdl:2060/20130010774. ISBN 978-1-62410-181-6.{{cite journal}}: CS1 maint: multiple names: authors list (link)

gltrs.grc.nasa.gov

S. Walston, A. Cetel, R. MacKay, K. O’Hara, D. Duhl, and R. Dreshfield (2004). Joint Development of a Fourth Generation Single Crystal Superalloy Archived 15 October 2006 at the Wayback Machine. NASA TM—2004-213062. December 2004. Retrieved: 16 June 2010.

patents.google.com

researchgate.net

Bhagi LK, Rastogi V, Gupta P (2017). "Study of corrosive fatigue and life enhancement of low pressure steam turbine blade using friction dampers". Journal of Mechanical Science and Technology. 31: 17–27. doi:10.1007/s12206-016-1203-5. S2CID 115023151.
https://www.researchgate.net/publication/267620184_Fundamental_Differences_Between_Conventional_and_Geared_Turbofans, Fig.1.5-14

sciencedirect.com

Acharya, Sumanta; Kanani, Yousef (2017-01-01), Sparrow, Ephraim M.; Abraham, John P.; Gorman, John M. (eds.), "Chapter Three - Advances in Film Cooling Heat Transfer", Advances in Heat Transfer, vol. 49, Elsevier, pp. 91–156, doi:10.1016/bs.aiht.2017.10.001, retrieved 2019-08-30
Goldstein, Richard J. (1971-01-01), "Film Cooling", in Irvine, Thomas F.; Hartnett, James P. (eds.), Advances in Heat Transfer Volume 7, vol. 7, Elsevier, pp. 321–379, doi:10.1016/s0065-2717(08)70020-0, ISBN 9780120200078, retrieved 2019-08-30
Bhagi LK, Rastogi V, Gupta P (2013).Fractographic investigations of the failure of L-1 low pressure steam turbine blade. Case Studies in Engineering Failure Analysis, 1(2), pp.72–78

scribd.com

Volume 1. Performance Flight Testing Phase. Chapter 7. Aero Propulsion page 7.122. Edwards Air Force Base, Air Force Test Center, February 1991. Size: 8MB. mirror of ADA320315.pdf

semanticscholar.org

api.semanticscholar.org

Bogard, D. G.; Thole, K. A. (2006-03-01). "Gas Turbine Film Cooling" (PDF). Journal of Propulsion and Power. 22 (2): 249–270. doi:10.2514/1.18034. S2CID 54063370. Archived from the original (PDF) on 2019-03-07.
Bhagi LK, Rastogi V, Gupta P (2017). "Study of corrosive fatigue and life enhancement of low pressure steam turbine blade using friction dampers". Journal of Mechanical Science and Technology. 31: 17–27. doi:10.1007/s12206-016-1203-5. S2CID 115023151.

pdfs.semanticscholar.org

Bogard, D. G.; Thole, K. A. (2006-03-01). "Gas Turbine Film Cooling" (PDF). Journal of Propulsion and Power. 22 (2): 249–270. doi:10.2514/1.18034. S2CID 54063370. Archived from the original (PDF) on 2019-03-07.

specialmetals.com

"Products." Archived 8 December 2012 at archive.today Special Metals. Retrieved: 5 March 2011.

st-ge-energy.com

Schilke, P. W. (2004). Advanced Gas Turbine Materials and Coatings^{[permanent dead link‍]}. GE Energy. August 2004. Retrieved: 25 May 2011.

steelforge.com

"Metal Tidbits: Nimonic." steelforge.com. Retrieved: 5 March 2011.

turboaerodesign.com

"Nomenclature of Cooled Axial Turbine Blade – Turbomachinery Aerodynamic Design".

turbomachinerymag.com

"Moving beyond the steam cooling".

umn.edu

me.umn.edu

What is Film Cooling?

upm.es

webserver.dmt.upm.es

Martinez, Isidoro. "Aircraft propulsion. Thermal and mechanical limitations in jet engines Archived 2015-07-01 at the Wayback Machine" page 19. Technical University of Madrid, School of Aeronautical Engineering, 2015. Retrieved: April 2015.

usgs.gov

minerals.usgs.gov

Magyar, Michael J. "Mineral Yearbook: Rhenium" (PDF). United States Geological Survey.

web.archive.org

Bogard, D. G.; Thole, K. A. (2006-03-01). "Gas Turbine Film Cooling" (PDF). Journal of Propulsion and Power. 22 (2): 249–270. doi:10.2514/1.18034. S2CID 54063370. Archived from the original (PDF) on 2019-03-07.
MacKay, Rebecca A., et al. (2007). Low-Density, Creep-Resistant Superalloys Developed for Turbine Blades. NASA Glenn's Research & Technology. Updated: 7 November 2007. Retrieved: 16 June 2010.
S. Walston, A. Cetel, R. MacKay, K. O’Hara, D. Duhl, and R. Dreshfield (2004). Joint Development of a Fourth Generation Single Crystal Superalloy Archived 15 October 2006 at the Wayback Machine. NASA TM—2004-213062. December 2004. Retrieved: 16 June 2010.
Volume 1. Performance Flight Testing Phase. Chapter 7. Aero Propulsion page 7.122. Edwards Air Force Base, Air Force Test Center, February 1991. Size: 8MB. mirror of ADA320315.pdf
Martinez, Isidoro. "Aircraft propulsion. Thermal and mechanical limitations in jet engines Archived 2015-07-01 at the Wayback Machine" page 19. Technical University of Madrid, School of Aeronautical Engineering, 2015. Retrieved: April 2015.

yumpu.com

https://www.yumpu.com/en/document/read/11154551/geared-fan-vki-aero-engine-design-mtu-aero-engines, p.15