Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / HECTOR; architecture of integrated rotorcraft multidisciplinary design and optimization framework, deployed for the design analysis and optimization of conceptual rotorcraft powerplant configurations Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) Reference PATM geographical definition; (b) time variations of deployed operational airspeed and altitude Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) Sensitivity analysis for various engine and mission output parameters against engine OPR, (b) sensitivity analysis for various engine and mission output parameters against HEE; conceptual regenerated Bo105 helicopter, PATM Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) RSM for engine SFC DP versus engine LPC PR and HPC PR, (b) RSM for mission NO x versus engine LPC PR and HPC PR; conceptual regenerated Bo105 helicopter, PATM Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) RSM for engine SFC DP versus engine HPC PR and HEE; (b) RSM for mission NO x versus engine HPC PR and HEE; conceptual regenerated Bo105 helicopter, PATM Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) RSM for EW versus engine W· and HEE, (b) Pareto front models corresponding to minimum MFB and minimum mission NO x inventory; conceptual regenerated Bo105 helicopter, PATM Figure Legend:

Date of download: 9/18/2016 Copyright © ASME. All rights reserved. From: Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact J. Eng. Gas Turbines Power. 2015;137(7): doi: / (a) Comparison between baseline and three selected Pareto front models; mission level parameters and deltas; Bo105 helicopter, PATM, (b) fuel flow production rate comparison between baseline and three selected Pareto front models, (c) NO x production rate comparison between baseline and three selected Pareto front models; conceptual regenerated Bo105 helicopter, PATM Figure Legend: