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1Academic Journal
المصدر: Xibei Gongye Daxue Xuebao, Vol 37, Iss 6, Pp 1231-1237 (2019)
مصطلحات موضوعية: em-ks algorithm, kalman filter smoothing, tvar, flutter boundary prediction, numerical simulation, flutter time domain criterion, Motor vehicles. Aeronautics. Astronautics, TL1-4050
وصف الملف: electronic resource
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2Academic Journal
المؤلفون: Zhongyu Liu, Xueyuan Nie, Guannan Zheng, Guowei Yang
المصدر: Applied Sciences, Vol 11, Iss 5389, p 5389 (2021)
مصطلحات موضوعية: CFD/CSD coupling, flutter boundary, computational aeroelasticity, Technology, Engineering (General). Civil engineering (General), TA1-2040, Biology (General), QH301-705.5, Physics, QC1-999, Chemistry, QD1-999
Relation: https://www.mdpi.com/2076-3417/11/12/5389; https://doaj.org/toc/2076-3417; https://doaj.org/article/15a66ba7dca445c8a456f2d75dc270f0
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3Conference
المؤلفون: Pecka, A., Bublík, O., Vimmr, J.
المساهمون: Adámek, Vítězslav, Jonášová, Alena, Plánička, Stanislav, Zajíček, Martin
مصطلحات موضوعية: třepetající se hranice, interakce struktura tekutina, aeroelastická analýza, FlowPro, Galerkinův kód, flutter boundary, fluid-structure interaction, aeroelastic analysis, Galerkin code
وصف الملف: 2 s.; application/pdf
Relation: Computational Mechanics; Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 83-84.; http://hdl.handle.net/11025/30819; https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf
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4Academic Journal
المؤلفون: Sung-Yeoul LEE
المصدر: Journal of Fluid Science and Technology, Vol 3, Iss 1, Pp 195-206 (2008)
مصطلحات موضوعية: aeroelasticity, limit cycle oscillation, flutter boundary, viscous effects, Science (General), Q1-390, Technology
وصف الملف: electronic resource
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5
المؤلفون: Shiqiang Duan, Junhao Liu, Hua Zheng, Chengming Pei
المصدر: Xibei Gongye Daxue Xuebao, Vol 37, Iss 6, Pp 1231-1237 (2019)
مصطلحات موضوعية: em-ks algorithm, Computer simulation, Stochastic process, Computer science, flutter boundary prediction, General Engineering, Boundary (topology), ComputerApplications_COMPUTERSINOTHERSYSTEMS, TL1-4050, Filter (signal processing), flutter time domain criterion, Physics::Fluid Dynamics, Variable (computer science), kalman filter smoothing, tvar, numerical simulation, Expectation–maximization algorithm, Flutter, Time domain, Algorithm, Motor vehicles. Aeronautics. Astronautics
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6Academic Journal
المؤلفون: Hiroshi TORII, Yuji MATSUZAKI, 松崎 雄嗣, 鳥居 弘志
المصدر: 日本航空宇宙学会誌 / Aeronautical and Space Sciences Japan. 1996, 44(511):473
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7Academic Journal
المؤلفون: Hiroshi MATSUSHITA, Jiro NAKAMICHI, Tetsuhiko UEDA, 上田 哲彦, 中道 二郎, 松下 洸
المصدر: 日本航空宇宙学会誌 / Aeronautical and Space Sciences Japan. 1996, 44(511):454
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8Dissertation/ Thesis
المؤلفون: Karnick, Pradeepa Tumkur
Thesis Advisors: Venkatraman, Kartik
مصطلحات موضوعية: Aerodynamics, Airfoil, Transonic Flutter, Shock-Boundry Layer, Airplanes, Turbulent Viscous Flow, Flutter Boundary, Shock Dynamics, Aeroelasticity, Euler Flow, Turbulence, Transonic Flow, Aerospace Engineering
Relation: G25863
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9
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10
المؤلفون: Kheirandish, Hamid Reza, Nakamichi, Jiro
المصدر: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :366-369
مصطلحات موضوعية: 超音速機, dynamic pressure, transonic flight, 計算流体力学, computational fluid dynamics, 非定常オイラー方程式, structural design, 遷音速領域, フラッタ境界, 空力弾性応答, vibration damping, エルロンフラッタ, 航空機設計, フラッタ, フラッタ速度, 線形理論, 遷音速飛行, aircraft design, flutter boundary, linear theory, unsteady Euler equation, 振動減衰, transonic region, aeroelastic response, research aircraft, 実験機, 構造設計, SST, flutter speed, 数値シミュレーション, aileron flutter, flutter, 動圧, numerical simulation, SST experimental aircraft, SST実験機, supersonic aircraft
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11
المؤلفون: Kanda, Atsushi, Kai, Takashi, Nakamura, Toshiya
المصدر: 宇宙航空研究開発機構特別資料: 第69回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 69th Meeting. :8-12
مصطلحات موضوعية: reentry vehicle, Mach number, 低超音速領域, マッハ数, 再突入機, 風洞試験, Physics::Fluid Dynamics, フラッタ境界, 圧力測定, low supersonic region, pressure measurement, DPM, 翼, wind tunnel test, wing, flutter boundary
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12
المؤلفون: Sun, Tianrui, Petrie-Repar, Paul, Qi, Di
المصدر: Proceedings of the ASME Turbo Expo.
مصطلحات موضوعية: Aerodynamic stability, Flutter, Steam turbine, Tip clearance, Aerodynamics, Computer software, Flutter (aerodynamics), Gas turbines, Leakage (fluid), Steam, Turbines, Turbomachine blades, Turbomachinery, Unsteady flow, Flutter boundary predictions, Numerical results, Numerical software, Structural frequencies, Tip clearance flow, Tip leakage vortex, Unsteady aerodynamics, Steam turbines
وصف الملف: print
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13
المؤلفون: Minegishi, Masakatsu, Ando, Yasukatsu, Matsuzaki, Yuji, Ejiri, Hiroshi, Noda, Junichi, Sekine, Hideo, Tate, Atsushi, Watanabe, Mitsunori
المصدر: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 693:1-8
مصطلحات موضوعية: flutter vibration frequency, 吹出式超音速風洞, blowdown supersonic wind tunnel, supersonic delta wing, 超音速吹出し, 風洞試験, 超音速デルタ翼, フラッタ振動数, supersonic blowdown, flutter prevention effect, フラッタ限界値測定, flutter emergency stopper, フラッタ緊急停止装置, flutter test, flutter boundary estimation, wind tunnel test, フラッタ試験, フラッタ抑止効果
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14
المؤلفون: Nakamichi, Jiro, Ejiri, Hiroshi, Kikuchi, Takao, Minegishi, Masakatsu, Sotozaki, Tokuo, Kumakura, Ikuo, Noguchi, Yoshio, Isogai, Koji
المصدر: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1208:1-12
مصطلحات موضوعية: 衝撃波失速フラッタ, aeroelastic scale model, 前進翼, 翼ダイバージェンス, 主翼空力設計, フラッタ限界, フラッタモード, wing divergence, shock stall flutter, aeroelastic tayloring, 空力弾性スケールモデル, 複合材箱型桁, 空力弾性最適化, aeroelastic optimization, wing aerodynamic design, flutter mode, 遷音速空気力学, flutter test, composite material box spar, swept forward wing, transonic aerodynamics, 空力弾性テーラリング, フラッタ試験, flutter boundary
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15
المؤلفون: Minegishi, Masakatu, Ando, Yasukatu, Matsuzaki, Yuji, Ejiri, Hiroshi, Sakakibara, Seizo, Noda, Jyunichi, Ishida, Kiyomichi, Sekine, Hideo, Tate, Atsushi, Watanabe, Mitsunori
المصدر: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1179:1-19
مصطلحات موضوعية: delta wing, 非定常不規則応答, フラッタ限界推定, protection device, 振動試験, 風洞試験, flutter characteristic, サブクリティカルフラッタ, 空力弾性, subcritical flutter, デルタ翼, フラッタ, flutter model, 時系列解析, model design, 模型設計, vibration characteristic, nonstationary random process, supersonic flow, 振動特性, 保護装置, aeroelasticity, flutter, フラッタ模型, flutter boundary estimation, 超音速流れ, wind tunnel test, aerodynamics, vibration test, フラッタ特性
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16
المؤلفون: Alex Loeven, Sunetra Sarkar, Jeroen A. S. Witteveen, Hester Bijl
المصدر: IndraStra Global.
مصطلحات موضوعية: Airfoil, Airfoils, Polynomial approximation, Galerkin polynomial chaos, Physics::Fluid Dynamics, Control theory, Uncertain systems, Stall flutter, Bifurcation, Uncertainty quantification, Mathematics, Parametric statistics, Stall indicators, Polynomial chaos, Mechanical Engineering, Flutter (aerodynamics), Mathematical analysis, Stall (fluid mechanics), Monte Carlo methods, Aeroelasticity, Galerkin methods, Probability distributions, Bifurcation (mathematics), Probabilistic collocation, Gas dynamics, Flutter, Uncertainty analysis, Flutter boundary, Aerodynamic center
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17
المؤلفون: Camilo, Elizangela
Thesis Advisors: Marques, Flávio Donizeti
مصطلحات موضوعية: Aeroelasticidade não linear, CFD methods, Escoamento transônico, Flutter boundary, Fronteiras de flutter, LCO, Métodos de CFD, Nonlinear aeroelasticity, Transonic flow
وصف الملف: application/pdf
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18Dissertation/ Thesis
المؤلفون: Elizangela Camilo
Thesis Advisors: Flávio Donizeti Marques, João Luiz Filgueiras de Azevedo, Paulo Celso Greco Junior, Roberto Gil Annes da Silva, Leandro Franco de Souza
المصدر: Biblioteca Digital de Teses e Dissertações da USPUniversidade de São PauloUSP.
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19
المؤلفون: ANDO, Yasukatsu, MATSUZAKI, Yuji, MINEGISHI, Masakatsu, EJIRI, Hiroshi, SAKAKIBARA, Seizo, NODA, Junichi, ISHIDA, Kiyomichi
المصدر: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1153. 1153:17
مصطلحات موضوعية: Supersonic delta wing, vibration-mode parameter, flutter boundary, stationary random response, autoregressive estimation method
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20Dissertation/ Thesis
المؤلفون: Karnick, Pradeepa Tumkur
المساهمون: Venkatraman, Kartik
مصطلحات موضوعية: Aerodynamics, Airfoil, Transonic Flutter, Shock-Boundry Layer, Airplanes, Turbulent Viscous Flow, Flutter Boundary, Shock Dynamics, Aeroelasticity, Euler Flow, Turbulence, Transonic Flow, Aerospace Engineering
وصف الملف: application/pdf
Relation: G25863; http://etd.iisc.ac.in/handle/2005/2688; http://etd.iisc.ac.in/static/etd/abstracts/3509/G25863-Abs.pdf