المؤلفون: Nicholas F. Giannelis, Tamas Bykerk, Gareth A. Vio

المصدر: Aerospace, Vol 10, Iss 9, p 746 (2023)

مصطلحات موضوعية: high angle of attack aerodynamics, delta-wings, vortical flows, computational fluid dynamics, experimental aerodynamics, benchmark aerodynamic models, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://www.mdpi.com/2226-4310/10/9/746Test; https://doaj.org/toc/2226-4310Test

الوصول الحر: https://doaj.org/article/8add2cf1ec6f4334b972047f4ca2282aTest

المؤلفون: Giannelis, Nicholas F., Bykerk, Tamas, Vio, Gareth A.

المساهمون: The University of Newcastle. College of Engineering, Science & Environment, School of Engineering

مصطلحات موضوعية: high angle of attack aerodynamics, delta-wings, vortical flows, computational fluid dynamics, experimental aerodynamics, benchmark aerodynamic models

العلاقة: Aerospace Vol. 10, Issue 9, no. 746; http://hdl.handle.net/1959.13/1491206Test; uon:53037

الإتاحة: http://hdl.handle.net/1959.13/1491206Test

المؤلفون: Petterson, Kristian

المساهمون: Poll, D. I. A., Sillén, M., Arlinger, B.

مصطلحات موضوعية: 629.13, High angle-of-attack aerodynamics, aerodynamics, combat aircraft, manoeuverability, vortical wake, forebody

الوصول الحر: https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.392234Test

المؤلفون: Kengo KANAMORI, Kengo MAEDA, Takashi MATSUNO, Yuki OKAMUNE, 前田 健吾, 岡宗 悠紀, 松野 隆, 金森 健吾

المصدر: The Proceedings of Conference of Chugoku-Shikoku Branch. 2013, 1

المؤلفون: Shigeru Yokouchi, Takashi Matsuno, Yoshiaki Nakamura, 中村 佳朗, 松野 隆, 横内 滋

المصدر: 日本航空宇宙学会論文集 / JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2004, 52(608):429

المؤلفون: Hirotoshi KUBOTA, 久保田 弘敏

المصدر: 日本航空宇宙学会誌 / Aeronautical and Space Sciences Japan. 1985, 33(377):360

المؤلفون: 空気力学部門委員会

المصدر: 日本航空宇宙学会誌 / Aeronautical and Space Sciences Japan. 1985, 33(377):380

المؤلفون: Rinoie, Kenichi, Fujita, Toshimi, Iwasaki, Akihito, Fujieda, Hirotoshi

المصدر: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1245:1-13

مصطلحات موضوعية: 超音速翼形状, oil flow visualization, low speed delta wing characteristic, ボルテックスフラップ, supersonic wing configuration, low speed wind tunnel test, デルタ翼空気力学, 高迎角空気力学, デルタ翼低速特性, 前縁剥離渦, leading edge device, デルタ翼揚抗比, 表面圧力計測, leading edge separation vortex, sweepback angle effect, 前縁デバイス, vortex flap, delta wing aerodynamics, delta wing lift to drag ratio, high angle of attack aerodynamics, 低速風洞試験, オイルフロー可視化, 後退翼効果, surface pressure measurement

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::69847808c9992f5fd937622950096216Test
http://id.nii.ac.jp/1696/00041216Test/

المؤلفون: Chen, XR, Deng, XY, Wang, YK, Liu, PW, Gu, ZF

المساهمون: Chen, XR (reprint author), Beijing Univ Aeronaut & Astronaut, Inst Fluid Mech, Beijing 100083, Peoples R China., Beijing Univ Aeronaut & Astronaut, Inst Fluid Mech, Beijing 100083, Peoples R China., Peking Univ, Dept Engn Sci & Mech, Beijing 100871, Peoples R China.

المصدر: SCI

مصطلحات موضوعية: asymmetric vortex, slender body of revolution, bistable flow, high angle of attack aerodynamics, VORTEX ASYMMETRY, OGIVE CYLINDER

العلاقة: ACTA MECHANICA SINICA.2002,18,(6),581-593.; 1013226; http://hdl.handle.net/20.500.11897/256372Test; WOS:000180359200003

الإتاحة: https://doi.org/20.500.11897/256372Test
https://hdl.handle.net/20.500.11897/256372Test

المؤلفون: Miroslav Mokry

المصدر: 42nd AIAA Aerospace Sciences Meeting and Exhibit.

مصطلحات موضوعية: Physics, Momentum (technical analysis), Optics, Interference (communication), business.industry, high angle of attack aerodynamics, wind tunnel wall interference, business, Computational physics

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0e9171f1c6ba74dc2a5b6810f3a26e95Test
https://doi.org/10.2514/6.2004-606Test