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1دورية أكاديمية
المؤلفون: Jianmiao Yi, Feng Deng
المصدر: Aerospace; Volume 10; Issue 7; Pages: 650
مصطلحات موضوعية: aerodynamic shape optimization, airfoil parameterization, thin-airfoil theory, deep learning, generative model
وصف الملف: application/pdf
العلاقة: Aeronautics; https://dx.doi.org/10.3390/aerospace10070650Test
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2تقرير
المؤلفون: Liu, Tianshu, 王士召, Liu, Hao, 何国威
المساهمون: Liu, Tianshu
مصطلحات موضوعية: Bird, Flight, Scaling, Flapping wing, Airfoil, Wing geometry, Wing kinematics, Aerodynamics, Vortex, Lift, Drag, Thrust, Thin-airfoil theory, Lifting-line theory, Wake models, Kutta-Joukowski theorem, Actuator disk model, Vortex ring model, CFD, Multiple joint arm system, LEADING-EDGE VORTEX, AVIAN WING GEOMETRY, GLIDING FLIGHT, WAKE STRUCTURE, ANIMAL FLIGHT, THRUSH NIGHTINGALE, FLAPPING FLIGHT, ENERGY SAVINGS, FLYING BIRDS, Engineering
العلاقة: PROGRESS IN AEROSPACE SCIENCES; http://dspace.imech.ac.cn/handle/311007/93779Test; http://dspace.imech.ac.cn/handle/311007/93780Test
الإتاحة: https://doi.org/10.1016/j.paerosci.2023.100933Test
http://dspace.imech.ac.cn/handle/311007/93779Test
http://dspace.imech.ac.cn/handle/311007/93780Test -
3دورية أكاديمية
المؤلفون: Shen, X, AVITAL, E, Rezaienia, MA, Paul, G, Alexander, T
مصطلحات موضوعية: Thin airfoil theory, surface curvature, boundary layer, aerodynamic efficiency
العلاقة: Journal of Algorithms and Computational Technology; http://qmro.qmul.ac.uk/xmlui/handle/123456789/16067Test
الإتاحة: https://doi.org/10.1177/1748301816665527Test
http://qmro.qmul.ac.uk/xmlui/handle/123456789/16067Test -
4دورية أكاديمية
المساهمون: Centre National de la Recherche Scientifique - CNRS (FRANCE), Institut National des Sciences Appliquées de Lyon - INSA (FRANCE), Office National d'Etudes et Recherches Aérospatiales - ONERA (FRANCE), Université Paris-Saclay (FRANCE), Université Claude Bernard-Lyon I - UCBL (FRANCE), Ecole Centrale de Lyon (FRANCE)
مصطلحات موضوعية: Acoustique, Turbulence, Cascade interaction, Fan-OGV broadband noise, Gusts, Synthetic turbulence, Computational aeroacoustics, Thin airfoil theory
وصف الملف: application/pdf
العلاقة: https://oatao.univ-toulouse.fr/24072/1/Polacsek_24072.pdfTest; Polacsek, Cyril and Clair, Vincent and Le Garrec, Thomas and Reboul, Gabriel and Jacob, Marc C. Numerical predictions of turbulence-cascade interaction noise using CAA with a stochastic model. (2015) AIAA Journal, 53 (12). 3551-3566. ISSN 0001-1452
الإتاحة: https://doi.org/10.2514/1.J053896Test
https://oatao.univ-toulouse.fr/24072Test/
https://oatao.univ-toulouse.fr/24072/1/Polacsek_24072.pdfTest -
5
المؤلفون: Kos, Matej
المساهمون: Matijašević, Dubravko
مصطلحات موضوعية: metoda konačnih volumena, teorija tankih aeroprofila, idealni napadni kut, Refleksni aeroprofili, Reflex airfoils, thin airfoil theory, srednja linija aeroprofila, finite volume method, TEHNIČKE ZNANOSTI. Zrakoplovstvo, raketna i svemirska tehnika, ideal angle of attack, TECHNICAL SCIENCES. Aviation, Rocket and Space Technology, mean camber line
وصف الملف: application/pdf
الوصول الحر: https://explore.openaire.eu/search/publication?articleId=od______9595::95f2ab72a9d5cbeb38db6d13fcad16cbTest
https://repozitorij.fsb.unizg.hr/islandora/object/fsb:6195/datastream/PDFTest -
6رسالة جامعية
المؤلفون: Kos, Matej
المساهمون: Matijašević, Dubravko
مصطلحات موضوعية: TEHNIČKE ZNANOSTI. Zrakoplovstvo, raketna i svemirska tehnika, TECHNICAL SCIENCES. Aviation, Rocket and Space Technology, Refleksni aeroprofili, teorija tankih aeroprofila, srednja linija aeroprofila, idealni napadni kut, metoda konačnih volumena, Reflex airfoils, thin airfoil theory, mean camber line, ideal angle of attack, finite volume method
وصف الملف: application/pdf
العلاقة: https://zir.nsk.hr/islandora/object/fsb:6195Test; https://urn.nsk.hr/urn:nbn:hr:235:391513Test; https://repozitorij.unizg.hr/islandora/object/fsb:6195Test; https://repozitorij.unizg.hr/islandora/object/fsb:6195/datastream/PDFTest
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7
المؤلفون: Vojković, Tea
المساهمون: Matijašević, Dubravko
مصطلحات موضوعية: Theodorsen function, Teorija tankih aeroprola, Thin airfoil theory, necirkulacijski tok, Teorija tankih aeroprofila, oscilatorno gibanje, necirkulacijski tok, cirkulacijski tok, Theodorsenova funkcija, cirkulacijski tok, circulatory flow, TEHNIČKE ZNANOSTI. Zrakoplovstvo, raketna i svemirska tehnika, oscilatory motion, TECHNICAL SCIENCES. Aviation, Rocket and Space Technology, Theodorsenova funkcija, oscilatorno gibanje, noncirculatory flow
وصف الملف: application/pdf
الوصول الحر: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::73c61fc2a685608b63139a970ee62696Test
https://www.bib.irb.hr/1077347Test -
8دورية أكاديمية
المؤلفون: Teruaki AKAMATSU, Yoshifumi OHGAMI, 大上 芳文, 赤松 映明
المصدر: 日本機械学会論文集 B編 / Transactions of the Japan Society of Mechanical Engineers Series B. 1986, 52(475):1014
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9رسالة جامعية
المؤلفون: 김소희
المساهمون: 최해천, 공과대학 기계항공공학부
مصطلحات موضوعية: Multirotor UAV, Large eddy simulation, Sectional lift coefficient, Sectional drag coefficient, Actuator momentum theory, Thin airfoil theory
الوقت: 621
وصف الملف: application/pdf; 1379467 bytes
العلاقة: 000000150213; http://hdl.handle.net/10371/141392Test
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10رسالة جامعية
المؤلفون: Vojković, Tea
المساهمون: Matijašević, Dubravko
مصطلحات موضوعية: TEHNIČKE ZNANOSTI. Zrakoplovstvo, raketna i svemirska tehnika, TECHNICAL SCIENCES. Aviation, Rocket and Space Technology, Teorija tankih aeroprola, oscilatorno gibanje, necirkulacijski tok, cirkulacijski tok, Theodorsenova funkcija, Thin airfoil theory, oscilatory motion, noncirculatory flow, circulatory flow, Theodorsen function
وصف الملف: application/pdf
العلاقة: https://zir.nsk.hr/islandora/object/fsb:4972Test; https://urn.nsk.hr/urn:nbn:hr:235:662014Test; https://repozitorij.unizg.hr/islandora/object/fsb:4972Test; https://repozitorij.unizg.hr/islandora/object/fsb:4972/datastream/PDFTest
