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1-4 of 4
Keywords: Turboprop
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Journal Articles
Comparative performance analysis of a turboprop engine used in regional aircraft by considering design and flight conditions
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2025) 97 (3): 345–355.
Published: 31 January 2025
...Onur Yuksel; Hakan Aygün Purpose This study aims to evaluate variation of performance metrics involving specific fuel consumption (SFC), thrust, thermal efficiency and overall efficiency values of turboprop engine used in regional aircraft according to varying altitude of 0–9 km and 0.3–0.6 Mach...
Journal Articles
Modeling of environmental effect factor and exergetic sustainability index with cuckoo search algorithm for a business jet
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2022) 94 (7): 1157–1169.
Published: 08 March 2022
... In this study, models were created to estimate ESI and EEF sustainability parameters in various flight phases for a business jet with a turboprop engine using the cuckoo search algorithm (CSA) method. The database used for modeling includes the various engine parameters (torque, engine airflow, gas generator...
Journal Articles
Real-time integrated turboprop take-off model under propeller-wing interaction
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Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (7): 917–926.
Published: 10 July 2019
...Yiwei Wang; Xianghua Huang; Jiaqin Huang Purpose The purpose of the paper is to build a real-time integrated turboprop take-off model which fully takes the interaction between diverse parts of aircraft into consideration. Turboprops have the advantage of short take-off distance derived from...
Journal Articles
Aerodynamic design of gas turbine engine intake duct
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Aircraft Engineering and Aerospace Technology: An International Journal (2016) 88 (5): 605–612.
Published: 05 September 2016
...Bambang I. Soemarwoto; Okko J. Boelens; Toni Kanakis Purpose The purpose of this paper is to provide a design solution of an engine intake duct suitable for delivering air to the compressor of a gas turbine engine of a general aviation turboprop aircraft, where the initial duct shape suffers...
