Investigation of exergetic and exergo‐sustainability metrics for high by‐pass turbofan engine at different power settings

Environmental Progress & Sustainable Energy ◽

10.1002/ep.13700 ◽

2021 ◽

Author(s):

Hakan Aygun

Keyword(s):

Sustainability Metrics ◽

Turbofan Engine

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An exergy way to quantify sustainability metrics for a high bypass turbofan engine

Energy ◽

10.1016/j.energy.2015.04.026 ◽

2015 ◽

Vol 86 ◽

pp. 722-736 ◽

Author(s):

Onder Turan

Keyword(s):

Sustainability Metrics ◽

Turbofan Engine

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Polymer Sustainability Metrics Compared

Chemical & Engineering News ◽

10.1021/cen093010164846 ◽

2010 ◽

pp. 10093010164846

Author(s):

Steve Ritter

Keyword(s):

Sustainability Metrics

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Turbofan Engine Performance Deterioration Due To Fan Erosion

International Review of Aerospace Engineering (IREASE) ◽

10.15866/irease.v12i2.16072 ◽

2019 ◽

Vol 12 (2) ◽

pp. 93

Author(s):

H. Z. Hassan ◽

M. H. Gobran ◽

A. F. El-Saied

Keyword(s):

Engine Performance ◽

Turbofan Engine ◽

Performance Deterioration

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Current status of development of the V2500 turbofan engine.

The Journal of the Japan Society of Aeronautical Engineering ◽

10.2322/jjsass1969.37.163 ◽

1989 ◽

Vol 37 (423) ◽

pp. 163-171

Author(s):

Mototsugu ITO

Keyword(s):

Current Status ◽

Turbofan Engine

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Scheduling Turbofan Engine Control Set Points by Semi-Infinite Optimization

10.23919/acc.1988.4790099 ◽

1988 ◽

Author(s):

D.M. Stimler

Keyword(s):

Engine Control ◽

Turbofan Engine ◽

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Applications of finite element and wave envelope element approximations to turbofan engine noise radiation including flight effects

10.2514/6.1984-2333 ◽

1984 ◽

Author(s):

A. PARRETT ◽

W. EVERSMAN

Keyword(s):

Finite Element ◽

Engine Noise ◽

Turbofan Engine ◽

Noise Radiation

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Evaluation of high speed turbojet/turbofan engine concepts on the performance of the DSL STS-booster stage

10.2514/6.1995-2750 ◽

1995 ◽

Author(s):

Martin Sippel ◽

Matthias Sodomann ◽

Frank Deidewig

Keyword(s):

Turbofan Engine

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Investigation of IGV trailing edge blowing in a F109 turbofan engine

10.2514/6.2000-224 ◽

2000 ◽

Author(s):

Jeffrey Kozak ◽

Wing Ng

Keyword(s):

Trailing Edge ◽

Turbofan Engine

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Withdrawal: Flow Field Analysis Inside First Stage Rotor (LPC) of Low By Pass Ratio Turbofan Engine With Integrated Aircraft Intake Data

AIAA Propulsion and Energy 2019 Forum ◽

10.2514/6.2019-4276.c1 ◽

2019 ◽

Author(s):

Aizaz Farooq ◽

Jehanzeb Masud ◽

Muhammad Usama Bin Shehzad

Keyword(s):

Field Analysis ◽

Turbofan Engine ◽

Flow Field Analysis

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THREE-DIMENSIONAL FLOW IN A TRANSONIC AXIAL FLOW FAN OF A HIGH BYPASS RATIO TURBOFAN ENGINE

International Conference on Aerospace Sciences and Aviation Technology ◽

10.21608/asat.2011.27139 ◽

2011 ◽

Vol 11 (ASAT CONFERENCE) ◽

pp. 1-21

Author(s):

A. ABD EL-AZIM ◽

M. GOBRAN ◽

H. HASSAN

Keyword(s):

Three Dimensional ◽

Axial Flow Fan ◽

Three Dimensional Flow ◽

Turbofan Engine ◽

Dimensional Flow ◽

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