A numerical investigation into the effect of engine bleed on performance of a single-spool turbojet engine

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 222, Issue 7, 2008, Pages 939-949

  Rahman, N U ^a   Whidborne, J F ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

Bleed flow; Component volume method; Engine performance; Turbojet simulation

Indexed keywords

AIRCRAFT; ELECTRIC GENERATORS; FLOW SIMULATION; GAS DYNAMICS; MACHINE DESIGN; REELS; TURBINES;

AERODYNAMIC CONTROL SURFACES; BLEED AIRS; BLEED FLOW; BLENDED WING BODIES; COMPONENT VOLUME METHOD; ENGINE PERFORMANCE; ENGINE SIMULATIONS; ENGINE SPEEDS; EXPERIMENTAL DATUMS; EXPERIMENTAL VALUES; INTEGRAL PARTS; MATLAB/SIMULINK; MICRO TURBINES; NUMERICAL INVESTIGATIONS; OLYMPUS; REAL-TIME SIMULATIONS; SIMULATION RESULTS; SLEW RATES; SPEED CONTROLLERS; STEADY STATES; TRANSIENT PERFORMANCES; TURBOJET SIMULATION; VOLUME METHODS;

ENGINES;

EID: 56549102635     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO389     Document Type: Article

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