First and second law analysis of future aircraft engines

Journal of Engineering for Gas Turbines and Power

Volumn 136, Issue 3, 2014, Pages

  Grönstedt, Tomas ^a   Irannezhad, Mohammad ^a   Lei, Xu ^a   Thulin, Oskar ^a   Lundbladh, Anders ^b  

^a CHALMERS UNIVERSITY OF TECHNOLOGY   (Sweden)

^b GKN Aerospace   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; THERMODYNAMICS; TURBOFAN ENGINES;

EXERGY DESTRUCTIONS; IRREVERSIBILITY RATE; PERFORMANCE BENEFITS; PERFORMANCE ENGINES; PERFORMANCE LEVEL; PULSE DETONATION COMBUSTION; SECOND LAW ANALYSIS; SECOND LAW OF THERMODYNAMICS;

ENGINES;

EID: 84903716716     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4025727     Document Type: Article

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