Razão de diluição (Portuguese Wikipedia)

Analysis of information sources in references of the Wikipedia article "Razão de diluição" in Portuguese language version.

refsWebsite

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4web.archive.org

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1britannica.com

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1books.google.com

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1animatedengines.com

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1flightglobal.com

223^rd place

550^th place

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1roadrunnersinternationale.com

low place

low place

abcm.org.br

«Archived copy» (PDF). Consultado em 25 de dezembro de 2016. Arquivado do original (PDF) em 16 de maio de 2017

animatedengines.com

Animated Engines

asme.org

proceedings.asmedigitalcollection.asme.org

Zipkin, M. A. (1984). «The PW1120: A High Performance, Low Risk F100 Derivative». Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. [S.l.: s.n.] ISBN 978-0-7918-7947-4. doi:10.1115/84-GT-230

books.google.com

Nag, P.K. "Basic And Applied Thermodynamics" p550. Published by Tata McGraw-Hill Education. Quote: "If the cowl is removed from the fan the result is a turboprop engine. Turbofan and turboprop engines differ mainly in their bypass ratio 5 or 6 for turbofans and as high as 100 for turboprop."

britannica.com

«Bypass ratio | engineering»

doi.org

dx.doi.org

Zipkin, M. A. (1984). «The PW1120: A High Performance, Low Risk F100 Derivative». Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. [S.l.: s.n.] ISBN 978-0-7918-7947-4. doi:10.1115/84-GT-230

flightglobal.com

«Archived copy». Consultado em 24 de dezembro de 2016. Arquivado do original em 24 de dezembro de 2016

mit.edu

web.mit.edu

Prof. Z. S. Spakovszky. "11.5 Trends in thermal and propulsive efficiency Archive" MIT turbines, 2002. Thermodynamics and Propulsion

roadrunnersinternationale.com

«Never Told Tales of Pratt & Whitney by Dr. Bob Abernethy»

stanford.edu

adg.stanford.edu

Ilan Kroo and Juan Alonso. "Aircraft Design: Synthesis and Analysis, Propulsion Systems: Basic Concepts Archive" Stanford University School of Engineering, Department of Aeronautics and Astronautics. Quote: "When the bypass ratio is increased to 10-20 for very efficient low speed performance, the weight and wetted area of the fan shroud (inlet) become large, and at some point it makes sense to eliminate it altogether. The fan then becomes a propeller and the engine is called a turboprop. Turboprop engines provide efficient power from low speeds up to as high as M=0.8 with bypass ratios of 50-100."

web.archive.org

Ilan Kroo and Juan Alonso. "Aircraft Design: Synthesis and Analysis, Propulsion Systems: Basic Concepts Archive" Stanford University School of Engineering, Department of Aeronautics and Astronautics. Quote: "When the bypass ratio is increased to 10-20 for very efficient low speed performance, the weight and wetted area of the fan shroud (inlet) become large, and at some point it makes sense to eliminate it altogether. The fan then becomes a propeller and the engine is called a turboprop. Turboprop engines provide efficient power from low speeds up to as high as M=0.8 with bypass ratios of 50-100."
Prof. Z. S. Spakovszky. "11.5 Trends in thermal and propulsive efficiency Archive" MIT turbines, 2002. Thermodynamics and Propulsion
«Archived copy» (PDF). Consultado em 25 de dezembro de 2016. Arquivado do original (PDF) em 16 de maio de 2017
«Archived copy». Consultado em 24 de dezembro de 2016. Arquivado do original em 24 de dezembro de 2016