FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2942299527> ?p ?o ?g. }

• W2942299527 endingPage "596" @default.
• W2942299527 startingPage "587" @default.
• W2942299527 abstract "Abstract One-dimensional modeling is considered as one of the most approved methods of studying the characteristics and performance of aircraft reciprocating engines, operating under different flight conditions. Owing to the recent progresses, the one-dimensional modeling of piston engine components including air filter, carburetor, air manifold, inlet and outlet valves, cylinder, piston, crankshaft, exhaust manifold, and turbocharger have become possible using some of the engineering software such as the GT-Power. The present paper is devoted to extensive performance analysis of one of the most widely used aircraft engines, the Rotax-914 which is a spark-ignition (SI) turbocharged aircraft engine, during the climb phase. The survey is conducted through the preparation of a one-dimensional model of the Rotax-914 using GT-power software. Then, to be more consistence with the real flight condition, its turbocharger is accurately modeled by considering the performance curves provided by the manufacturer. Next, to ensure its accuracy, the developed model was validated against the manufacturer data. The important engine performance parameters and turbocharger performance curves were analyzed for different flight aspects up to 30,000 feet. The obtained results indicated that the turbocharger prevents a dramatic decline in engine performance parameters up to 18,000 feet. Thereafter, the compressor reaches the choking region, fails to supply air demand, leading to extreme performance loss. The effect of ambient temperature difference from the international-standard-atmosphere (ISA) on engine performance was also investigated. A 40 °C increase in the ambient temperature causes a 10% drop in the brake horsepower and consequently, a performance loss was observed during the climb. Ambient temperature and altitude differently affect engine performance. The effect of ambient temperature on the engine performance was greater as the compressor reaches the choking region. Beyond the choking region, altitude variations had a greater impact on engine performance than the temperature variations." @default.
• W2942299527 created "2019-05-03" @default.
• W2942299527 creator A5081980193 @default.
• W2942299527 creator A5091410447 @default.
• W2942299527 date "2019-06-01" @default.
• W2942299527 modified "2023-10-17" @default.
• W2942299527 title "Performance prediction of aircraft gasoline turbocharged engine at high-altitudes" @default.
• W2942299527 cites W1506053686 @default.
• W2942299527 cites W1582616156 @default.
• W2942299527 cites W1980257732 @default.
• W2942299527 cites W2006990571 @default.
• W2942299527 cites W2037519657 @default.
• W2942299527 cites W2055996333 @default.
• W2942299527 cites W2056711788 @default.
• W2942299527 cites W2188866599 @default.
• W2942299527 cites W2324981417 @default.
• W2942299527 cites W2521878538 @default.
• W2942299527 cites W2753947932 @default.
• W2942299527 cites W2758195806 @default.
• W2942299527 cites W2896787309 @default.
• W2942299527 cites W2898756271 @default.
• W2942299527 cites W589874635 @default.
• W2942299527 doi "https://doi.org/10.1016/j.applthermaleng.2019.04.116" @default.
• W2942299527 hasPublicationYear "2019" @default.
• W2942299527 type Work @default.
• W2942299527 sameAs 2942299527 @default.
• W2942299527 citedByCount "13" @default.
• W2942299527 countsByYear W29422995272020 @default.
• W2942299527 countsByYear W29422995272021 @default.
• W2942299527 countsByYear W29422995272022 @default.
• W2942299527 countsByYear W29422995272023 @default.
• W2942299527 crossrefType "journal-article" @default.
• W2942299527 hasAuthorship W2942299527A5081980193 @default.
• W2942299527 hasAuthorship W2942299527A5091410447 @default.
• W2942299527 hasConcept C103697071 @default.
• W2942299527 hasConcept C127413603 @default.
• W2942299527 hasConcept C131097465 @default.
• W2942299527 hasConcept C146978453 @default.
• W2942299527 hasConcept C171146098 @default.
• W2942299527 hasConcept C178802073 @default.
• W2942299527 hasConcept C21541133 @default.
• W2942299527 hasConcept C39432304 @default.
• W2942299527 hasConcept C39573554 @default.
• W2942299527 hasConcept C511840579 @default.
• W2942299527 hasConcept C548081761 @default.
• W2942299527 hasConceptScore W2942299527C103697071 @default.
• W2942299527 hasConceptScore W2942299527C127413603 @default.
• W2942299527 hasConceptScore W2942299527C131097465 @default.
• W2942299527 hasConceptScore W2942299527C146978453 @default.
• W2942299527 hasConceptScore W2942299527C171146098 @default.
• W2942299527 hasConceptScore W2942299527C178802073 @default.
• W2942299527 hasConceptScore W2942299527C21541133 @default.
• W2942299527 hasConceptScore W2942299527C39432304 @default.
• W2942299527 hasConceptScore W2942299527C39573554 @default.
• W2942299527 hasConceptScore W2942299527C511840579 @default.
• W2942299527 hasConceptScore W2942299527C548081761 @default.
• W2942299527 hasLocation W29422995271 @default.
• W2942299527 hasOpenAccess W2942299527 @default.
• W2942299527 hasPrimaryLocation W29422995271 @default.
• W2942299527 hasRelatedWork W1501853650 @default.
• W2942299527 hasRelatedWork W2278026893 @default.
• W2942299527 hasRelatedWork W2331859824 @default.
• W2942299527 hasRelatedWork W2601034667 @default.
• W2942299527 hasRelatedWork W2788198102 @default.
• W2942299527 hasRelatedWork W2803391259 @default.
• W2942299527 hasRelatedWork W2891481963 @default.
• W2942299527 hasRelatedWork W2941663270 @default.
• W2942299527 hasRelatedWork W3032826303 @default.
• W2942299527 hasRelatedWork W3207069843 @default.
• W2942299527 hasVolume "156" @default.
• W2942299527 isParatext "false" @default.
• W2942299527 isRetracted "false" @default.
• W2942299527 magId "2942299527" @default.
• W2942299527 workType "article" @default.