Performance of small-scale aero-derivative industrial gas turbines derived from helicopter engines

Author:

Nkoi Barinyima,Pilidis Pericles,Nikolaidis Theoklis

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference22 articles.

1. Performance assessment of simple and modified cycle turboshaft gas turbines;Nkoi;Propulsion and Power Research,2013

2. P.P. Walsh, P. Fletcher, Gas Turbine Performance, Second ed., Blackwell Publishing, 2004, p. 38.

3. B. Bellis, Turbo-shaft engines, about.com guide, 〈http://inventors.about.com/od/jstartinventions/ss/jet_engine_4.htm〉 [cited 28 June 2012].

4. D. Dilba, Pioneering new core engine technologies. MTU Aero Engines, MTU Aero Engines Holding AG., 〈http://www.mtu.de/en/takeoff/report/archive_old/2_2010/210_newac/index.html〉 [cited 6 September 2012].

5. M.D. Paramour, M.J. Sapsard, Future technology and requirements for helicopter Engines, in: W.A. Stewart (Ed.), NATO-AGARD conference on helicopter propulsion systems - AGARD-CP-302, Toulouse, France, 11–14 May 1981, pp. 4-1–4-6.

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