Matches in SemOpenAlex for { <https://semopenalex.org/work/W4309213020> ?p ?o ?g. }
Showing items 1 to 75 of
75
with 100 items per page.
- W4309213020 endingPage "15076" @default.
- W4309213020 startingPage "15076" @default.
- W4309213020 abstract "Due to the dynamic development of environmentally friendly aircraft propulsion, the paper describes the effect of distributed propulsion on the emission and fuel consumption changes of aircraft in comparison to aircraft with traditional propulsion. A distributed propulsion is a propulsion composed of a set of units located on the leading edges of the wings or on the fuselage, generating a thrust symmetrically distributed on both sides of the fuselage. The analysis was based on the technical data of AOS H2 motor glider. During the tests for the adopted geometry of distributed propulsion, the improvement of airframe aerodynamic parameters was determined by conducting a CFD flow analysis. Based on the energy method, the flight range and duration were determined for the aircraft with distributed propulsion. It occurred that they increased by 19% compared to the initial variant—traditional propulsion. For the adopted energy source—Wankel AG-407TGi engine, the emissions of CO, CO2, and NO in the exhausts were measured. After the application of distributed propulsion, the emissions and fuel consumption were reduced by 16%. The research conducted showed that the application of distributed propulsion instead of traditional propulsion can bring measurable environmental benefits. Conducting further research on multi-criteria optimization of aircraft structures may bring further benefits in terms of improving aircraft performance and environmentally friendly indicators." @default.
- W4309213020 created "2022-11-24" @default.
- W4309213020 creator A5014331320 @default.
- W4309213020 creator A5061486294 @default.
- W4309213020 creator A5072042967 @default.
- W4309213020 date "2022-11-14" @default.
- W4309213020 modified "2023-10-14" @default.
- W4309213020 title "Comparison of Pollutants Emission for Hybrid Aircraft with Traditional and Multi-Propeller Distributed Propulsion" @default.
- W4309213020 cites W1980329558 @default.
- W4309213020 cites W2156352249 @default.
- W4309213020 cites W2307620388 @default.
- W4309213020 cites W2751253715 @default.
- W4309213020 cites W2889476638 @default.
- W4309213020 cites W3042320565 @default.
- W4309213020 cites W3066824953 @default.
- W4309213020 cites W3082568103 @default.
- W4309213020 cites W3149958101 @default.
- W4309213020 cites W3157055926 @default.
- W4309213020 cites W4200278194 @default.
- W4309213020 cites W3183417544 @default.
- W4309213020 doi "https://doi.org/10.3390/su142215076" @default.
- W4309213020 hasPublicationYear "2022" @default.
- W4309213020 type Work @default.
- W4309213020 citedByCount "1" @default.
- W4309213020 countsByYear W43092130202023 @default.
- W4309213020 crossrefType "journal-article" @default.
- W4309213020 hasAuthorship W4309213020A5014331320 @default.
- W4309213020 hasAuthorship W4309213020A5061486294 @default.
- W4309213020 hasAuthorship W4309213020A5072042967 @default.
- W4309213020 hasBestOaLocation W43092130201 @default.
- W4309213020 hasConcept C1034443 @default.
- W4309213020 hasConcept C113556839 @default.
- W4309213020 hasConcept C127413603 @default.
- W4309213020 hasConcept C146978453 @default.
- W4309213020 hasConcept C171146098 @default.
- W4309213020 hasConcept C199104240 @default.
- W4309213020 hasConcept C204323151 @default.
- W4309213020 hasConcept C205167488 @default.
- W4309213020 hasConcept C39432304 @default.
- W4309213020 hasConcept C45882903 @default.
- W4309213020 hasConcept C62200009 @default.
- W4309213020 hasConcept C79420006 @default.
- W4309213020 hasConceptScore W4309213020C1034443 @default.
- W4309213020 hasConceptScore W4309213020C113556839 @default.
- W4309213020 hasConceptScore W4309213020C127413603 @default.
- W4309213020 hasConceptScore W4309213020C146978453 @default.
- W4309213020 hasConceptScore W4309213020C171146098 @default.
- W4309213020 hasConceptScore W4309213020C199104240 @default.
- W4309213020 hasConceptScore W4309213020C204323151 @default.
- W4309213020 hasConceptScore W4309213020C205167488 @default.
- W4309213020 hasConceptScore W4309213020C39432304 @default.
- W4309213020 hasConceptScore W4309213020C45882903 @default.
- W4309213020 hasConceptScore W4309213020C62200009 @default.
- W4309213020 hasConceptScore W4309213020C79420006 @default.
- W4309213020 hasFunder F4320318271 @default.
- W4309213020 hasIssue "22" @default.
- W4309213020 hasLocation W43092130201 @default.
- W4309213020 hasOpenAccess W4309213020 @default.
- W4309213020 hasPrimaryLocation W43092130201 @default.
- W4309213020 hasRelatedWork W1552033611 @default.
- W4309213020 hasRelatedWork W2069102467 @default.
- W4309213020 hasRelatedWork W2071265826 @default.
- W4309213020 hasRelatedWork W2208032779 @default.
- W4309213020 hasRelatedWork W4205214618 @default.
- W4309213020 hasRelatedWork W4234909587 @default.
- W4309213020 hasRelatedWork W4280625557 @default.
- W4309213020 hasRelatedWork W4309213020 @default.
- W4309213020 hasRelatedWork W814162367 @default.
- W4309213020 hasRelatedWork W820053666 @default.
- W4309213020 hasVolume "14" @default.
- W4309213020 isParatext "false" @default.
- W4309213020 isRetracted "false" @default.
- W4309213020 workType "article" @default.