المؤلفون: Ahmad Reza Ghasemi, Hamid Rabieyan-Najafabadi, Hossein Nejatbakhsh, Amin Gharaei

المصدر: Mechanics of Advanced Composite Structures, Vol 11, Iss 2, Pp 351-362 (2024)

مصطلحات موضوعية: composite c-spar, flutter speed, aeroelastic instability, aircraft tail, airfoil section, Mechanics of engineering. Applied mechanics, TA349-359

وصف الملف: electronic resource

Relation: https://macs.semnan.ac.ir/article_8424_03ea85cad4cfe2323a518b6706bc017e.pdf; https://doaj.org/toc/2423-4826; https://doaj.org/toc/2423-7043

URL الوصول: https://doaj.org/article/4c9ac2c1cfdb4774a2ce7925b8faa6c3

المؤلفون: Жданов , Олександр Іванович, Сущенко , Ольга Андріївна, Орлянський, Валерій Валентинович

المصدر: Electronics and Control Systems; Vol. 3 No. 81 (2024); 82-88 ; Электроника и системы управления; Том 3 № 81 (2024); 82-88 ; Електроніка та системи управління; Том 3 № 81 (2024); 82-88 ; 1990-5548

مصطلحات موضوعية: airfoil section, volume vortex generator, wind tunnel, aerodynamic characteristics, aerodynamic quality, experiment, профіль крила, об’ємний вихроутворювач, аеродинамічна труба, аеродинамічні характеристики, аеродинамічна якість, експеримент

وصف الملف: application/pdf

Relation: https://jrnl.nau.edu.ua/index.php/ESU/article/view/19041/26282; https://jrnl.nau.edu.ua/index.php/ESU/article/view/19041

الاتاحة: https://jrnl.nau.edu.ua/index.php/ESU/article/view/19041
https://doi.org/10.18372/1990-5548.81.19041

المؤلفون: Meskell, Craig, Pellegrino, Alberto

مصطلحات موضوعية: pitching two-dimensional airfoil section, Wind turbines, Wind turbine blades

Relation: International Journal of Aerospace Engineering; 2019; 6919505; Meskell, C. and Pellegrino, A., Vortex shedding lock-in due to pitching oscillation of a wind turbine blade section at high angles of attack, International Journal of Aerospace Engineering, 2019, 6919505, 2019; Y; https://www.hindawi.com/journals/ijae/2019/6919505/; http://hdl.handle.net/2262/89575; http://people.tcd.ie/cmeskell; 205582; http://dx.doi.org/10.1155/2019/6919505; orcid:0000-0001-6303-2796

الاتاحة: http://hdl.handle.net/2262/89575
https://www.hindawi.com/journals/ijae/2019/6919505/
http://people.tcd.ie/cmeskell
https://doi.org/10.1155/2019/6919505

المؤلفون: AK KARTIGESH A/L KALAI CHELVEN, HUSSAIN H. AL-KAYIEM

المصدر: Journal of Engineering Science and Technology, Vol 6, Iss 3, Pp 369-381 (2011)

مصطلحات موضوعية: NACA4412, Airfoil Section, Collision, Aerodynamic characteristics, Wings, Wing in ground effect, Engineering (General). Civil engineering (General), TA1-2040, Technology (General), T1-995

وصف الملف: electronic resource

Relation: http://jestec.taylors.edu.my/Vol%206%20Issue%203%20Junel%2011/Vol_6(3)_369_381_KAYIEM.pdf; https://doaj.org/toc/1823-4690

URL الوصول: https://doaj.org/article/a8dfffcc314f4ff48e5dea7de47dc85a

المؤلفون: Akari TSUDA, Kazuhiro IZUI, Keita KAMBAYASHI, Masato TAMAYAMA, Nozomu KOGISO, Shinji NISHIWAKI, Takayuki YAMADA, 上林 恵太, 小木曽 望, 山田 崇恭, 泉井 一浩, 津田 明, 玉山 雅人, 西脇 眞二

المصدر: 航空宇宙技術 / AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2019, 18:151

المصدر: 航空宇宙技術. 18:151-159

مصطلحات موضوعية: Morphing Wing, Airfoil Section, Structural Design, Multi-layered Compliant Mechanisms, Level Set-based Topology Optimization

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::7aba53af4130e12f74b16a8cb7c63d81
http://hdl.handle.net/10466/00017108

المؤلفون: Kambayashi, Keita, Tsuda, Akari, Kogiso, Nozomu, Yamada, Takayuki, Izui, Kazuhiro, Nishiwaki, Shinji, Tamayama, Masato

المصدر: 航空宇宙技術. 18:151-159

مصطلحات موضوعية: Morphing Wing, Airfoil Section, Structural Design, Multi-layered Compliant Mechanisms, Level Set-based Topology Optimization

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::5c48054140e86486d746432e6d0e3ab1
http://id.nii.ac.jp/1696/00046389/

المؤلفون: Katsuyoshi FUKIBA, Kazushi SATO, Nobuyuki TSUBOI, 佐藤 一志, 吹場 活佳, 坪井 伸幸

المصدر: 日本航空宇宙学会論文集 / JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2016, 64(3):153

المؤلفون: 上林 恵太, 津田 明, 小木曽 望, 山田 崇恭, 泉井 一浩, 西脇 眞二, 玉山 雅人

مصطلحات موضوعية: Morphing Wing, Airfoil Section, Structural Design, Multi-layered Compliant Mechanisms, Level Set-based Topology Optimization

وصف الملف: application/pdf

Relation: https://doi.org/10.2322/astj.JSASS-D-18-00062; https://omu.repo.nii.ac.jp/?action=repository_uri&item_id=12002; http://hdl.handle.net/10466/00017108; 航空宇宙技術. 2019, 18, P.151-159; 航空宇宙技術, 18, 151-159(2019-07-27); https://omu.repo.nii.ac.jp/?action=repository_action_common_download&item_id=12002&item_no=1&attribute_id=19&file_no=1

الاتاحة: http://hdl.handle.net/10466/00017108
https://omu.repo.nii.ac.jp/?action=repository_uri&item_id=12002
https://omu.repo.nii.ac.jp/?action=repository_action_common_download&item_id=12002&item_no=1&attribute_id=19&file_no=1

المؤلفون: Keiji KAWACHI, 河内 啓二

المصدر: 可視化情報学会誌 / Journal of the Visualization Society of Japan. 2000, 20(1Supplement):5

المؤلفون: Karam Y. Maalawi, Mervat A. Badr

المصدر: The Proceedings of the International Conference on Power Engineering (ICOPE). 2003, 61

المؤلفون: Katsumi HIRAOKA, Nobuyuki ARAI, 平岡 克己, 新井 啓之

المصدر: 日本航空宇宙学会論文集 / JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2009, 57(662):98

المؤلفون: Keiji KAWACHI, 河内 啓二

المصدر: 生物物理 / Seibutsu Butsuri. 1999, 39(5):279

المؤلفون: Akio ICHIKAWA, 市川 明夫

المصدر: 日本航空宇宙学会誌 / Aeronautical and Space Sciences Japan. 1992, 40(457):119

المؤلفون: Rafiee, M. (M.), Nitzsche, F. (Fred), Labrosse, M.R. (M. R.)

المصدر: International Journal of Applied Mechanics

مصطلحات موضوعية: airfoil section, Carbon nanotubes, cross-section design, fiber-reinforced nanocomposite, multiscale composites, VABS

Relation: https://ir.library.carleton.ca/pub/18296

الاتاحة: https://ir.library.carleton.ca/pub/18296
https://doi.org/10.1142/S1758825118500321

المؤلفون: Mohamed Sellam, Rachid Bessaïh, Amer Chpoun, N. Bekka

المساهمون: Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE), Department of Mechanical Engineering, Université Mentouri Constantine [Algérie] (UMC), Université frères Mentouri Constantine I (UMC)

المصدر: Numerical Heat Transfer, Part A Applications
Numerical Heat Transfer, Part A Applications, Taylor & Francis, 2009, 56 (12), pp.946--969. ⟨10.1080/10407780903508005⟩
Numerical Heat Transfer, Part A Applications, 2009, 56 (12), pp.946--969. ⟨10.1080/10407780903508005⟩

مصطلحات موضوعية: Airfoil, K-epsilon turbulence model, Flux difference splitting scheme, Airfoil section, 02 engineering and technology, K-omega turbulence model, 01 natural sciences, Upper surface, 010305 fluids & plasmas, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph], FASTRAN, Experiment data, 0203 mechanical engineering, 0103 physical sciences, Aerodynamic efficiency, Time integration, Baldwin Lomax model, Space discretizations, Low Reynolds number, Numerical investigations, Physics, Numerical Analysis, Angle of attack, Turbulence, Small scale, Temperature differences, Spalart-Allmaras, Turbulence modeling, Reynolds stress equation model, One-equation, Mechanics, Fully implicit scheme, Condensed Matter Physics, Chord lengths, Lift (force), 020303 mechanical engineering & transports, Classical mechanics, Numerical studies, Two equation, Numerical results, High order

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d7d43c3957ba91a2cd473e2ef29de4a7
https://hal.archives-ouvertes.fr/hal-01179797

المؤلفون: Jarvis, J. B., Selberg, B. P.

المصدر: Mechanical and Aerospace Engineering Faculty Research & Creative Works

مصطلحات موضوعية: Airfoil Section, Anhedral, Induced Drag, Momentum Intgral, Taper Ratios, Tip Chord, Viscous Drag, Wing Sail, Aerospace Engineering, Mechanical Engineering

Relation: https://scholarsmine.mst.edu/mec_aereng_facwork/2076; https://doi.org/10.4271/951432

الاتاحة: https://scholarsmine.mst.edu/mec_aereng_facwork/2076
https://doi.org/10.4271/951432

المؤلفون: Scarbrough, William T.

المصدر: Theses

مصطلحات موضوعية: Airfoil section generation

وصف الملف: application/pdf

Relation: https://scholarworks.rit.edu/theses/1285; https://scholarworks.rit.edu/context/theses/article/2289/viewcontent/WScarbroughThesis04_28_1992.pdf

الاتاحة: https://scholarworks.rit.edu/theses/1285
https://scholarworks.rit.edu/context/theses/article/2289/viewcontent/WScarbroughThesis04_28_1992.pdf

المؤلفون: Kamiya, Nobuhiko

المصدر: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:179-180

مصطلحات موضوعية: 鳥瞰図, hysteresis phenomenon, bird's eye view, angle of attack, 失速型特徴, シンポジウム, practical range, Reynolds number, 数値シミュレーション, NACA9324, numerical simulation, stalling characteristic, 翼断面, ヒステリシス現象, 迎角, airfoil section, 実用領域, symposium, レイノルズ数

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::83ede7b0cc009916ab385a8e5653d6a0
http://id.nii.ac.jp/1696/00041328/

المؤلفون: Van Dyke, Milton D.

المساهمون: Ames Aeronautical Laboratory (U.S.)

مصطلحات موضوعية: airfoils, airfoil-section theory

وصف الملف: 50 p.; Text

Relation: local-cont-no: 93R13379; url: http://hdl.handle.net/2060/19930084089; rep-no: NACA-TN-3390; casi: 19930084089; https://digital.library.unt.edu/ark:/67531/metadc57381/; ark: ark:/67531/metadc57381

الاتاحة: https://digital.library.unt.edu/ark:/67531/metadc57381/