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Title:Aerodynamic analysis of an oscillating airfoil in a power-extraction regime using the compressible Navier-Stokes equations with efficient and accurate low-speed preconditioning
Authors:ID Drofelnik, Jernej (Author)
ID Škerget, Leopold (Mentor) More about this mentor... New window
ID Campobasso, Sergio (Comentor)
Files:.pdf UNI_Drofelnik_Jernej_2012.pdf (2,40 MB)
MD5: DE9AB7038188A8C3B7C4CCD7FF1CC4D5
PID: 20.500.12556/dkum/f3868526-6e52-47fc-b0d1-97c86d946463
 
Language:English
Work type:Undergraduate thesis
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Abstract:A wing that is simultaneously heaving and pitching may extract energy from an oncoming air flow, thus acting as turbine. The purpose of this study was to analyse the relationship between the aerodynamics and the theoretical performance of this device by means of timedependent laminar flow simulations performed with a research compressible finite volume Navier-Stokes solver COSA. In presented analyses, which confirm the findings of another independent study, the efficiency of the power extraction of this device can be of the order of 35 %, and such an efficient operating condition is characterized due to the favourable effects of a strong dynamic stall. This study is a part of a wider research programme of Dr. Campobasso’s group at University of Glasgow, aiming to develop a general-purpose computational framework for unsteady aerodynamic and aeroacoustic wind energy engineering. In view of aeroacoustic applications, the developed flow solver uses the compressible formulation of the Navier-Stokes equations with carefully optimized low-speed preconditioning. To demonstrate the modeling capabilities, the accuracy and the high computational performance of the developed low-speed preconditioning technology, the unsteady aerodynamics of the energy-extracting device is simulated by using a computationally challenging freestream Mach number of 0.001. A mixed preconditioning strategy that maintains both the nominal accuracy and the computational efficiency of the solver also for time-dependent low-speed problems is presented. A fundamental element of novelty of this study is a thorough assessment of the proposed approach partly based on the challenging and realistic problem associated with the oscillating wing device.
Keywords:Low-speed preconditioning, compressible multigrid Navier-Stokes solver, energy-extracting oscillating wing, computational fluid dynamics.
Place of publishing:Maribor
Publisher:[J. Drofelnik]
Year of publishing:2012
PID:20.500.12556/DKUM-36807 New window
UDC:533.6.011.8(043.2)
COBISS.SI-ID:16974614 New window
NUK URN:URN:SI:UM:DK:1GY2HVQH
Publication date in DKUM:06.07.2012
Views:2801
Downloads:195
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FS
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Secondary language

Language:Slovenian
Title:Aerodinamična analiza nihajočega krila v energijsko-ekstrakcijskem režimu z uporabo stisljivih Navier-Stokesovih enačb z učinkovitim in natančnim nizko-hitrostnim predpogojevalnikom
Abstract:V zračnem toku nihajoče krilo, ki se sočasno nagiba okrog prečne osi, lahko deluje kot turbina. Namen študije je analiza odvisnosti aerodinamike in teoretične zmogljivosti te naprave s pomočjo časovno-odvisnih laminarnih tokovnih simulacij, izvedenih z akademskim programskim paketom COSA, ki uporablja formulacijo Navier-Stokesovih enačb nestacionarnega gibanja newtonske viskozne stisljive tekočine na osnovi metode končnih volumnov. Analiza potrjuje ugotovitve druge neodvisne študije, da lahko ta naprava dosega izkoristke v območju 35 %. Dober izkoristek je posledica ugodnih učinkov močnega odtrganja zračnega toka iz krila. Študija je del širšega raziskovalnega programa, ki ga vodi Dr. Campobasso na Univerzi v Glasgowu, ki razvija splošen programski sestav za reševanje problemov nestacionarne aerodinamike in aeroakustike vetrno-energijskega inženiringa. Glede na aeroakustične aplikacije uporablja COSA Navier-Stokesove enačbe za stisljivo tekočino s skrbno oblikovanim nizko-hitrostnim predpogojevalnikom. Za demonstracijo zmožnosti, natančnosti in visoke računske zmogljivosti razvite nizko-hitrostne predpogojevalne tehnologije, je bila simulirana nestacionarna aerodinamika energijsko-ekstrakcijske naprave, z uporabo zahtevnega prosto-tokovnega Machovega števila 0.001. Predstavljena je strategija mešanega nizkohitrostnega predpogojevalnika, ki vzdržuje nominalno natančnost in računsko učinkovitost programskega paketa tudi za časovno-odvisne nizko-hitrostne probleme. Bistvena novost je temeljita ocena predlaganega pristopa, delno zasnovanega na zahtevnem in realističnem problemu, povezanem z napravo z nihajočim krilom.
Keywords:Nizko-hitrostni predpogojevalnik, večmrežna metoda, Navier-Stokesov programski paket za stisljivo tekočino, energijsko-ekstrakcijsko nihajoče krilo, računalniška dinamika tekočin.


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