Recuperated gas turbine aeroengines. Part III: engine concepts for reduced emissions, lower fuel consumption, and noise abatement-Reference-Cited by-同舟云学术

Recuperated gas turbine aeroengines. Part III: engine concepts for reduced emissions, lower fuel consumption, and noise abatement

Published:2008-07-04 Issue:4 Volume:80 Page:408-426
ISSN:0002-2667
Container-title:Aircraft Engineering and Aerospace Technology
language:en
Short-container-title:Aircraft Eng & Aerospace Tech

Author:

McDonald Colin F.,Massardo Aristide F.,Rodgers Colin,Stone Aubrey

Publisher

Emerald

Reference18 articles.

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2. Barrie, D. (2007), “Engine limits”,Aviation Week & Space Technology, April 2, p. 52.

3. Bennett, H.W. (1983), “Aero engine development for the future”,I.Mech.E. Power Industries Division Proceedings, Vol. 197 No. 48.

4. Elliott, S. (1994), “Commercial turbofans”,Flight International, June, p. 38.

5. Ferrato, M. and Thonon, B. (1997), “A compact ceramic plate‐fin heat exchanger for gas turbine heat recovery”,Proceedings of Compact Heat Exchanger Meeting, Snowbird, UT, pp. 195‐9.

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