Development of an open rotor cycle model in NPSS using a multi-design point approach

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2011, Pages 441-450

  Hendricks, Eric S ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DESIGNS; AVIATION PROJECTS; COUNTER ROTATING; COUNTER-ROTATING PROPELLERS; CYCLE ANALYSIS; CYCLE MODEL; DESIGN POINTS; ENGINE EMISSION; ENVIRONMENTALLY RESPONSIBLE; FREESTREAM MACH NUMBER; FUTURE GENERATIONS; MODELING CAPABILITIES; NUMERICAL PROPULSION SYSTEM; OPEN ROTORS; PERFORMANCE MAPS; POINT APPROACH; POTENTIAL BENEFITS; POTENTIAL IMPACTS; POWER MANAGEMENT SCHEME; POWER TURBINES; PROPELLER BLADES; SUBSONIC AIRCRAFT; TECHNIQUES USED;

AERODYNAMICS; AIRCRAFT ENGINES; ALTERNATIVE FUELS; ENERGY MANAGEMENT; EXHIBITIONS; FIXED WINGS; MACH NUMBER; NASA; PROPELLERS; TURBINE COMPONENTS;

COMPUTER SIMULATION;

EID: 84865505938     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2011-46694     Document Type: Conference Paper

References (21)

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