FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2955782607> ?p ?o ?g. }

• W2955782607 endingPage "50" @default.
• W2955782607 startingPage "45" @default.
• W2955782607 abstract "The shape of the aerofoil determines how the air circulates around it and how much moment and force will be the acting on it. When the body is rigid (fixed) flow around the geometry remains unchanged at particular A.O.A. (angle of attack), but if the body is allowed to be flexible (free) i.e., it can deform its shape, due to which there will be a significant change in the shape of geometry that consequently changes the motion of air flow around it altering the moment and forces generated. This will led to a change in the distribution of pressure on the flexible membrane causing the A.O.A. to vary, due to which wing’s geometrical shape try to adopt it accordingly by forming a luff. This luff is mostly formed from the leading edge i.e., due to the membrane’s elastic nature; in the flow to adjust change prevailed. A computational approach was made to understand this effect. This was the main purpose of the project to be carried out. The dissertation mainly focuses onto understand the effect of flexibility on aerodynamics and performance of wing compared to the normal rigid wing section using the most simplified case for long term goal of finding out the behavior of aerodynamics on wings of pterosaur with and without fairing (soft membrane). The study was carried out by taking into account a specific case of pterosaur’s gliding flight at a speed of 33.3 m/s. This project included two test cases firstly, the rigid wing and secondly the flexible membrane wing, which were tested for both steady and unsteady viscous incompressible flows. For both the test cases it was considered that tension is mainly dominated by elastic strain (∏ 1 ). Both the test cases were carried out at fixed Reynolds’s number of 1.087 ´ 10 5 and Mach number 0.098. Use of equation similar to the bending of beam equation which is often referred as “Young Laplace Equation” was incorporated, that was modeled to a discrete formulation using second order accurate finite difference scheme. When the membrane of the wing was considered flexible there was a significant effect on forces generated, which in turn had an effect on performance in terms of coefficient of lift. Finally, comparisons between performances based on coefficient of lift of both test cases were carried out. The results obtained shows that the coefficient of lift for flexible case increased by 40% when compared to the rigid wing. Keywords: Young Laplace Equation, flexible wing, pterosaur wing, wing concept, morphing Cite this Article Milan Patel, Nikunj Mashru. Effect of Flexibility on Aircraft Wing. Journal of Aerospace Engineering and Technology. 2016; 6(1): 45–50p." @default.
• W2955782607 created "2019-07-12" @default.
• W2955782607 creator A5036064820 @default.
• W2955782607 creator A5083633863 @default.
• W2955782607 date "2016-05-11" @default.
• W2955782607 modified "2023-09-23" @default.
• W2955782607 title "Effect of Flexibility on Aircraft Wing" @default.
• W2955782607 doi "https://doi.org/10.37591/.v6i1.573" @default.
• W2955782607 hasPublicationYear "2016" @default.
• W2955782607 type Work @default.
• W2955782607 sameAs 2955782607 @default.
• W2955782607 citedByCount "0" @default.
• W2955782607 crossrefType "journal-article" @default.
• W2955782607 hasAuthorship W2955782607A5036064820 @default.
• W2955782607 hasAuthorship W2955782607A5083633863 @default.
• W2955782607 hasConcept C105795698 @default.
• W2955782607 hasConcept C107779570 @default.
• W2955782607 hasConcept C112124176 @default.
• W2955782607 hasConcept C121332964 @default.
• W2955782607 hasConcept C127413603 @default.
• W2955782607 hasConcept C132557482 @default.
• W2955782607 hasConcept C13393347 @default.
• W2955782607 hasConcept C137990359 @default.
• W2955782607 hasConcept C140820882 @default.
• W2955782607 hasConcept C179254644 @default.
• W2955782607 hasConcept C2524010 @default.
• W2955782607 hasConcept C2779570065 @default.
• W2955782607 hasConcept C2780598303 @default.
• W2955782607 hasConcept C28317120 @default.
• W2955782607 hasConcept C33923547 @default.
• W2955782607 hasConcept C38349280 @default.
• W2955782607 hasConcept C527307 @default.
• W2955782607 hasConcept C57879066 @default.
• W2955782607 hasConcept C66938386 @default.
• W2955782607 hasConcept C74650414 @default.
• W2955782607 hasConcept C97257150 @default.
• W2955782607 hasConceptScore W2955782607C105795698 @default.
• W2955782607 hasConceptScore W2955782607C107779570 @default.
• W2955782607 hasConceptScore W2955782607C112124176 @default.
• W2955782607 hasConceptScore W2955782607C121332964 @default.
• W2955782607 hasConceptScore W2955782607C127413603 @default.
• W2955782607 hasConceptScore W2955782607C132557482 @default.
• W2955782607 hasConceptScore W2955782607C13393347 @default.
• W2955782607 hasConceptScore W2955782607C137990359 @default.
• W2955782607 hasConceptScore W2955782607C140820882 @default.
• W2955782607 hasConceptScore W2955782607C179254644 @default.
• W2955782607 hasConceptScore W2955782607C2524010 @default.
• W2955782607 hasConceptScore W2955782607C2779570065 @default.
• W2955782607 hasConceptScore W2955782607C2780598303 @default.
• W2955782607 hasConceptScore W2955782607C28317120 @default.
• W2955782607 hasConceptScore W2955782607C33923547 @default.
• W2955782607 hasConceptScore W2955782607C38349280 @default.
• W2955782607 hasConceptScore W2955782607C527307 @default.
• W2955782607 hasConceptScore W2955782607C57879066 @default.
• W2955782607 hasConceptScore W2955782607C66938386 @default.
• W2955782607 hasConceptScore W2955782607C74650414 @default.
• W2955782607 hasConceptScore W2955782607C97257150 @default.
• W2955782607 hasIssue "1" @default.
• W2955782607 hasLocation W29557826071 @default.
• W2955782607 hasOpenAccess W2955782607 @default.
• W2955782607 hasPrimaryLocation W29557826071 @default.
• W2955782607 hasRelatedWork W1174905758 @default.
• W2955782607 hasRelatedWork W152828792 @default.
• W2955782607 hasRelatedWork W1567018296 @default.
• W2955782607 hasRelatedWork W1594345068 @default.
• W2955782607 hasRelatedWork W1980126543 @default.
• W2955782607 hasRelatedWork W2054608049 @default.
• W2955782607 hasRelatedWork W2070737565 @default.
• W2955782607 hasRelatedWork W2088365292 @default.
• W2955782607 hasRelatedWork W224318723 @default.
• W2955782607 hasRelatedWork W2323902977 @default.
• W2955782607 hasRelatedWork W2383789444 @default.
• W2955782607 hasRelatedWork W2402003641 @default.
• W2955782607 hasRelatedWork W2602816305 @default.
• W2955782607 hasRelatedWork W2734708847 @default.
• W2955782607 hasRelatedWork W2803433122 @default.
• W2955782607 hasRelatedWork W2886754068 @default.
• W2955782607 hasRelatedWork W310818794 @default.
• W2955782607 hasRelatedWork W378171844 @default.
• W2955782607 hasRelatedWork W647807127 @default.
• W2955782607 hasRelatedWork W85527973 @default.
• W2955782607 hasVolume "6" @default.
• W2955782607 isParatext "false" @default.
• W2955782607 isRetracted "false" @default.
• W2955782607 magId "2955782607" @default.
• W2955782607 workType "article" @default.