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Future trends in commercial aviation engines' combustion
HC Mongia - Novel combustion concepts for sustainable energy …, 2014 - Springer
This article gives an overview of the current rich-dome combustion system design,
requirements and challenges; followed by the first alternative to rich-domes that have been …
requirements and challenges; followed by the first alternative to rich-domes that have been …
N+ 3 and N+ 4 generation aeropropulsion engine combustors: Part 6: operating conditions, target goals and lifted jets
HC Mongia - 49th AIAA/ASME/SAE/ASEE Joint …, 2013 - arc.aiaa.org
This paper summarizes academically simulated takeoff and cruise operating conditions for
the N+ 3 and N+ 4 generation combustion systems and comparison likewise with the N and …
the N+ 3 and N+ 4 generation combustion systems and comparison likewise with the N and …
Innovative Approaches for Reducing CO2 Emissions of Aviation Engines Part 2: NPSS calibration with existing gas turbine engines
Innovative approaches for significantly reducing the aviation Greenhouse Gas (GHG)
emission need to be evaluated based on simple calculation methodology, viz. Numerical …
emission need to be evaluated based on simple calculation methodology, viz. Numerical …
[PDF][PDF] N+ 3 and N+ 4 Generation Aeropropulsion Engine Combustors: Part 1—Large Engines' Emissions
HC Mongia - Turbo Expo: Power for Land, Sea, and Air, 2013 - Citeseer
ABSTRACT A comprehensive assessment of emissions characteristics of the 1st, N and N+
1 generation rich-dome combustion products has been done to identify the lowest emissions …
1 generation rich-dome combustion products has been done to identify the lowest emissions …
Innovative approaches for reducing CO2 emissions of aviation engines part 1: selection of promising approaches
Innovative approaches for significantly reducing the aviation Greenhouse Gas (GHG)
emission need to be evaluated based on simple calculation methodology, viz. Numerical …
emission need to be evaluated based on simple calculation methodology, viz. Numerical …
N+ 3 and N+ 4 generation aeropropulsion engine combustors part 5: NOx, CO, HC and smoke emissions
HC Mongia - 49th AIAA/ASME/SAE/ASEE Joint …, 2013 - arc.aiaa.org
Previous studies showed that the rich-dome takeoff NOxEI technology status of small,
medium and large engines is presented well by the following expression: 𝑁𝑁𝑁𝑁𝑁= 0.04× …
medium and large engines is presented well by the following expression: 𝑁𝑁𝑁𝑁𝑁= 0.04× …
Conceptual design of aeropropulsion engine heat exchangers Part 1: micro channels and selection of advanced configurations
ABSTRACT A major challenge which emerged while looking at approaches for reduction of
aviation Greenhouse Gas (GHG) emissions was the design of a core exhaust heat recovery …
aviation Greenhouse Gas (GHG) emissions was the design of a core exhaust heat recovery …
N+ 3 and N+ 4 Generation Aeropropulsion Engine Combustors: Part 4: Specific Fuel Burn and Co2 Emissions
HC Mongia - 49th AIAA/ASME/SAE/ASEE Joint …, 2013 - arc.aiaa.org
The certified ICAO engine emissions database can be used for conducting comparative
assessment on the fuel burn advances made by the major OEM's during the last forty years …
assessment on the fuel burn advances made by the major OEM's during the last forty years …
Analysis on Turbine Cooling Air Bleeding of Intercooled Recuperated Turbofan Engine
H Gong, Z Wang, L Zhou… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
In order to further improve the intercooled recuperated turbofan engine (IRT) performance,
the possible high pressure turbine (HPT) cooling air bleeding schemes were analyzed …
the possible high pressure turbine (HPT) cooling air bleeding schemes were analyzed …