Zobrazeno 1 - 10
of 21
pro vyhledávání: '"airfoil data"'
Publikováno v:
Alexandria Engineering Journal, Vol 55, Iss 3, Pp 2035-2043 (2016)
This paper aims to optimize the distribution of chord and twist angle of small wind turbine blade in order to maximize its Annual Energy Production (AEP). A horizontal-axis wind turbine (HAWT) blade is optimized using a calculation code based on the
Externí odkaz:
https://doaj.org/article/c6ee5c0e210149c28e02c030010397af
Publikováno v:
Alexandria Engineering Journal, Vol 55, Iss 3, Pp 2035-2043 (2016)
This paper aims to optimize the distribution of chord and twist angle of small wind turbine blade in order to maximize its Annual Energy Production (AEP). A horizontal-axis wind turbine (HAWT) blade is optimized using a calculation code based on the
A propeller was designed using 2D airfoil data obtained from a panel method numeric code. The propeller was designed to operate at 75% chord based Reynolds number of 20k. At low Reynolds numbers 81% in each of the designed propellers.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::724720741c23ceee1b39f6c5791d78f0
Over the last three decades and a half, there has been huge effort to develop high performance propellers suitable for flight in the rarefied Mars atmosphere. This paper describes work undertaken in validating vortex theory in the design of a 2-blade
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5d72c4cde12938e1da8c0420cfc5b4a9
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Publikováno v:
Abdallah, I, Natarajan, A & Sørensen, J D 2013, Predicting the Extreme Loads on a Wind Turbine Considering Uncertainty in Airfoil Data . in G Deodatis, B R Ellingwood & D M Frangopol (eds), Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures : Proceedings of the 11th international conference on structural safety and reliability . CRC Press, pp. 39, Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures, New York, United States, 16/06/2013 .
Abdallah, I, Natarajan, A & Sørensen, J D 2014, Predicting the Extreme Loads on a Wind Turbine Considering Uncertainty in Airfoil Data . in G Deodatis, B R Ellingwood & D M Frangopol (eds), Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures : Proceedings of the 11th international conference on structural safety and reliability . CRC Press, pp. 215–222, Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures, New York, United States, 16/06/2013 . https://doi.org/10.1201/b16387-30
Abdallah, I, Natarajan, A & Sørensen, J D 2014, Predicting the Extreme Loads on a Wind Turbine Considering Uncertainty in Airfoil Data . in G Deodatis, B R Ellingwood & D M Frangopol (eds), Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures : Proceedings of the 11th international conference on structural safety and reliability . CRC Press, pp. 215–222, Safety, Reliability, Risk and Life-Cycle Performance of Structures and Infrastructures, New York, United States, 16/06/2013 . https://doi.org/10.1201/b16387-30
The sources contributing to uncertainty in a wind turbine blade static airfoil data include wind tunnel testing, CFD calculations, 3D rotational corrections based on CFD or emprircal models, surface roughness corrections, Reynolds number corrections,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a00615b4db2289ad8439b5903ceb52c8
https://vbn.aau.dk/da/publications/365b8d17-6af8-4bd2-a14c-22eccc398a4a
https://vbn.aau.dk/da/publications/365b8d17-6af8-4bd2-a14c-22eccc398a4a
Autor:
Sudani, Norikazu, Matsuno, Ken-ichi, Kanda, Hiroshi, Sato, Mamoru, Miwa, Hitoshi, Kawamoto, Iwao
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. :1-137
BGK No.1翼型に関する対応風洞試験が航空宇宙技術研究所(NAL)とカナダ国立航空研究所(IAR,旧NAE)の高レイノルズ数遷音速翼型試験設備において実施された。試験はレイノルズ数(翼弦長基準)2
Publikováno v:
航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集 = Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics. 19:63-68
航空宇宙技術研究所 10-12 Jun. 1992 東京 日本
National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan
ヘリコプタ用翼型の高迎角時の流れ場をシミュレートする手法を開発する目的で、ナビエ・
National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan
ヘリコプタ用翼型の高迎角時の流れ場をシミュレートする手法を開発する目的で、ナビエ・
Akademický článek
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Akademický článek
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