Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft

This paper describes the design, numerical analyses, and wind tunnel tests of the scaled model of a propeller serving as a propulsive element for the experimental tests of an advanced regional turboprop aircraft with engines installed on the horizontal tailplane tips. The design has been performed b...

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Main Authors: Danilo Ciliberti, Fabrizio Nicolosi
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/5/264
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author Danilo Ciliberti
Fabrizio Nicolosi
author_facet Danilo Ciliberti
Fabrizio Nicolosi
author_sort Danilo Ciliberti
collection DOAJ
description This paper describes the design, numerical analyses, and wind tunnel tests of the scaled model of a propeller serving as a propulsive element for the experimental tests of an advanced regional turboprop aircraft with engines installed on the horizontal tailplane tips. The design has been performed by complying with the thrust similarity from the full-scale aircraft propulsive requirements. Numerical analyses with a high-fidelity aerodynamic solver confirmed that the initial design made with XROTOR would achieve the expected performance. Finally, a strengthened version of the propeller has been manufactured via 3D printing and tested in the wind tunnel. Test data include measurements of thrust as well as propeller normal force at different angles of attack. Good agreement between numerical and experimental results has been observed, enabling the propeller to be used confidently in the aircraft wind tunnel powered test campaign.
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spelling doaj.art-bc91e7f1e11841d4ba9e902ef0dc61172023-11-23T09:38:05ZengMDPI AGAerospace2226-43102022-05-019526410.3390/aerospace9050264Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop AircraftDanilo Ciliberti0Fabrizio Nicolosi1Department of Industrial Engineering, University of Naples “Federico II”, Via Claudio 21, 80125 Naples, ItalyDepartment of Industrial Engineering, University of Naples “Federico II”, Via Claudio 21, 80125 Naples, ItalyThis paper describes the design, numerical analyses, and wind tunnel tests of the scaled model of a propeller serving as a propulsive element for the experimental tests of an advanced regional turboprop aircraft with engines installed on the horizontal tailplane tips. The design has been performed by complying with the thrust similarity from the full-scale aircraft propulsive requirements. Numerical analyses with a high-fidelity aerodynamic solver confirmed that the initial design made with XROTOR would achieve the expected performance. Finally, a strengthened version of the propeller has been manufactured via 3D printing and tested in the wind tunnel. Test data include measurements of thrust as well as propeller normal force at different angles of attack. Good agreement between numerical and experimental results has been observed, enabling the propeller to be used confidently in the aircraft wind tunnel powered test campaign.https://www.mdpi.com/2226-4310/9/5/264powered wind tunnel testpropeller designaerodynamicsaircraft stability and controlelectric motor
spellingShingle Danilo Ciliberti
Fabrizio Nicolosi
Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
Aerospace
powered wind tunnel test
propeller design
aerodynamics
aircraft stability and control
electric motor
title Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
title_full Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
title_fullStr Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
title_full_unstemmed Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
title_short Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
title_sort design analysis and testing of a scaled propeller for an innovative regional turboprop aircraft
topic powered wind tunnel test
propeller design
aerodynamics
aircraft stability and control
electric motor
url https://www.mdpi.com/2226-4310/9/5/264
work_keys_str_mv AT danilociliberti designanalysisandtestingofascaledpropellerforaninnovativeregionalturbopropaircraft
AT fabrizionicolosi designanalysisandtestingofascaledpropellerforaninnovativeregionalturbopropaircraft