Flight characteristic comparison of single- and dual-stage turbocharging reciprocating gasoline engine propeller propulsion system based on mathematical model-Reference-Cited by-同舟云学术

Flight characteristic comparison of single- and dual-stage turbocharging reciprocating gasoline engine propeller propulsion system based on mathematical model

Published:2016-05 Issue:5 Volume:30 Page:2369-2377
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Zhou Yicheng,Shan Peng

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-016-0447-4.pdf

Reference9 articles.

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2. J. Harp, Turbocharger system development and propulsion system testing, Prepared for Development Sciences Inc. under Contract No. DSI-80-TR-SC-05-A, ThermoMechanical Systems, Canoga Park CA, USA (1982) (declassified 1994).

3. C. Rodgers, Turbocharging a high altitude UAV C.I. Engine, AIAA Paper 2001-3970, USA (2001).

4. T. Korakianitis and T. Sadoi, Turbocharger-design effects on gasoline-engine performance, J. of Engineering for Gas Turbines and Power, Transactions of the ASME, 127 (3) (2005) 525–530.

5. J. L. Loth, G. J. Morris and P. B. Metlapalli, Staged turbocharging for high altitude IC engines, AIAA Paper 1997-3970, USA (1997).

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