Matches in SemOpenAlex for { <https://semopenalex.org/work/W2570978085> ?p ?o ?g. }
Showing items 1 to 89 of
89
with 100 items per page.
- W2570978085 endingPage "2" @default.
- W2570978085 startingPage "2" @default.
- W2570978085 abstract "An analysis of 2D subsonic flow over an NACA 0015 airfoil with a 30% trailing edge flap at a constant Reynolds number of 106 for various incidence angles and a range of flap deflections is presented. The steady-state governing equations of continuity and momentum conservation are solved combined with the realizable k-ε turbulence model using the ANSYS-Fluent code (Version 13.7, ANSYS, Inc., Canonsburg, PA, USA). The primary objective of the study is to provide a comprehensive understanding of flow characteristics around the NACA 0015 airfoil as a function of the angle of attack and flap deflection at Re = 106 using the realizable k-ε turbulence model. The results are validated through comparison of the predictions with the free field experimental measurements. Consistent with the experimental observations, the numerical results show that increased flap deflections increase the maximum lift coefficient, move the zero-lift angle of attack (AoA) to a more negative value, decrease the stall AoA, while the slope of the lift curve remains unchanged and the curve just shifts upwards. In addition, the numerical simulations provide limits for lift increment Δ C l and Cl, max values to be 1.1 and 2.2, respectively, obtained at a flap deflection of 50°. This investigation demonstrates that the realizable k-ε turbulence model is capable of predicting flow features over an airfoil with and without flap deflections with reasonable accuracy." @default.
- W2570978085 created "2017-01-13" @default.
- W2570978085 creator A5031241305 @default.
- W2570978085 creator A5043539201 @default.
- W2570978085 creator A5064117164 @default.
- W2570978085 date "2017-01-05" @default.
- W2570978085 modified "2023-10-18" @default.
- W2570978085 title "RANS Simulations of Aerodynamic Performance of NACA 0015 Flapped Airfoil" @default.
- W2570978085 cites W1977294541 @default.
- W2570978085 cites W1979319343 @default.
- W2570978085 cites W1995736581 @default.
- W2570978085 cites W2017621606 @default.
- W2570978085 cites W2032777079 @default.
- W2570978085 cites W2050370297 @default.
- W2570978085 cites W2093469257 @default.
- W2570978085 cites W4238157276 @default.
- W2570978085 cites W4246423323 @default.
- W2570978085 doi "https://doi.org/10.3390/fluids2010002" @default.
- W2570978085 hasPublicationYear "2017" @default.
- W2570978085 type Work @default.
- W2570978085 sameAs 2570978085 @default.
- W2570978085 citedByCount "14" @default.
- W2570978085 countsByYear W25709780852018 @default.
- W2570978085 countsByYear W25709780852019 @default.
- W2570978085 countsByYear W25709780852020 @default.
- W2570978085 countsByYear W25709780852021 @default.
- W2570978085 countsByYear W25709780852022 @default.
- W2570978085 countsByYear W25709780852023 @default.
- W2570978085 crossrefType "journal-article" @default.
- W2570978085 hasAuthorship W2570978085A5031241305 @default.
- W2570978085 hasAuthorship W2570978085A5043539201 @default.
- W2570978085 hasAuthorship W2570978085A5064117164 @default.
- W2570978085 hasBestOaLocation W25709780851 @default.
- W2570978085 hasConcept C112124176 @default.
- W2570978085 hasConcept C121332964 @default.
- W2570978085 hasConcept C124101348 @default.
- W2570978085 hasConcept C13393347 @default.
- W2570978085 hasConcept C139002025 @default.
- W2570978085 hasConcept C150486481 @default.
- W2570978085 hasConcept C182748727 @default.
- W2570978085 hasConcept C189360488 @default.
- W2570978085 hasConcept C196558001 @default.
- W2570978085 hasConcept C2781355719 @default.
- W2570978085 hasConcept C28317120 @default.
- W2570978085 hasConcept C32526432 @default.
- W2570978085 hasConcept C41008148 @default.
- W2570978085 hasConcept C527307 @default.
- W2570978085 hasConcept C57879066 @default.
- W2570978085 hasConcept C5804382 @default.
- W2570978085 hasConcept C74650414 @default.
- W2570978085 hasConceptScore W2570978085C112124176 @default.
- W2570978085 hasConceptScore W2570978085C121332964 @default.
- W2570978085 hasConceptScore W2570978085C124101348 @default.
- W2570978085 hasConceptScore W2570978085C13393347 @default.
- W2570978085 hasConceptScore W2570978085C139002025 @default.
- W2570978085 hasConceptScore W2570978085C150486481 @default.
- W2570978085 hasConceptScore W2570978085C182748727 @default.
- W2570978085 hasConceptScore W2570978085C189360488 @default.
- W2570978085 hasConceptScore W2570978085C196558001 @default.
- W2570978085 hasConceptScore W2570978085C2781355719 @default.
- W2570978085 hasConceptScore W2570978085C28317120 @default.
- W2570978085 hasConceptScore W2570978085C32526432 @default.
- W2570978085 hasConceptScore W2570978085C41008148 @default.
- W2570978085 hasConceptScore W2570978085C527307 @default.
- W2570978085 hasConceptScore W2570978085C57879066 @default.
- W2570978085 hasConceptScore W2570978085C5804382 @default.
- W2570978085 hasConceptScore W2570978085C74650414 @default.
- W2570978085 hasIssue "1" @default.
- W2570978085 hasLocation W25709780851 @default.
- W2570978085 hasLocation W25709780852 @default.
- W2570978085 hasOpenAccess W2570978085 @default.
- W2570978085 hasPrimaryLocation W25709780851 @default.
- W2570978085 hasRelatedWork W1991119176 @default.
- W2570978085 hasRelatedWork W2086092047 @default.
- W2570978085 hasRelatedWork W2333888770 @default.
- W2570978085 hasRelatedWork W2570978085 @default.
- W2570978085 hasRelatedWork W3028118390 @default.
- W2570978085 hasRelatedWork W3202792229 @default.
- W2570978085 hasRelatedWork W4221130345 @default.
- W2570978085 hasRelatedWork W811910245 @default.
- W2570978085 hasRelatedWork W1593489955 @default.
- W2570978085 hasRelatedWork W2753084040 @default.
- W2570978085 hasVolume "2" @default.
- W2570978085 isParatext "false" @default.
- W2570978085 isRetracted "false" @default.
- W2570978085 magId "2570978085" @default.
- W2570978085 workType "article" @default.