المؤلفون: Hidetsugu YOSHIDA, Toshihiko SUGAI

المصدر: Proceedings of the General Meeting of the Association of Japanese Geographers. 2005, :89

المؤلفون: Sakaue, Shoji, Nishioka, Michio

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). :61-66

مصطلحات موضوعية: Tollmien-Schlichting wave, flat plate, 超音速機, 平板, TVD scheme, Stokes層, 計算流体力学, 超音速流, computational fluid dynamics, TVDスキーム, two dimensional flow, supersonic flow, 層流境界層, 2次元流, Tollmien-Schlichting波, Stokes layer, 航空機設計, laminar boundary layer, supersonic aircraft, aircraft design

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::4e97b9a7986b18c32f3fc8e02ba56b84Test
http://id.nii.ac.jp/1696/00005734Test/

المؤلفون: Zhang, Wanqiu, Matsushima, Kisa, Iwamiya, Toshiyuki

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). :286-291

مصطلحات موضوعية: 逆翼設計, 超音速機, 空力学, thickness constraint control, 計算流体力学, 翼型設計, computational fluid dynamics, 自然層流翼, 厚さ制約制御, 翼型プロフィル, 翼断面形状, 積分方程式, airfoil profile, 層流境界層, 航空機設計, wing design, laminar boundary layer, aircraft design, 設計制約, 超音速実験機, 胴翼構成, 圧力分布, research aircraft, 実験機, pressure distribution, body-wing configuration, wing section geometry, aerodynamic characteristic, integral equation, wing planform, supersonic experimental airplane, 翼平面形, 空力特性, inverse wing design, natural laminar flow wing, aerodynamics, supersonic aircraft, design constraint

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::7d4ed4e2326919cf1fcad1f9fa117b8dTest
http://id.nii.ac.jp/1696/00005757Test/

المؤلفون: Jeong, Shinkyu, Matsushima, Kisa, Iwamiya, Toshiyuki, Obayashi, Shigeru

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). :78-83

مصطلحات موضوعية: Mach number, 超音速機, 民間航空, 計算流体力学, 胴翼結合, マッハ数, 圧力分布, computational fluid dynamics, design optimization, pressure distribution, 設計最適化, civil aviation, 層流境界層, 反復解法, iterative solution, 航空機設計, wing-fuselage combination, laminar boundary layer, supersonic aircraft, aircraft design

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::d4b0792f036f0026efac19a30ba25d38Test
http://id.nii.ac.jp/1696/00005737Test/

المؤلفون: Yoshida, Kenji, Iwamiya, Toshiyuki, Ueda, Yoshine, Ishikawa, Hiroaki

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). :280-285

مصطلحات موضوعية: e(exp N) method, 超音速機, 計算流体力学, computational fluid dynamics, 自然層流翼, 層流境界層, 付着線コンタミネーション, 航空機設計, e(exp N)法, laminar boundary layer, boundary layer transition, aircraft design, 境界層遷移, 超音速実験機, 圧縮性効果, 圧縮性境界層, 圧力分布, design optimization, research aircraft, 実験機, compressible boundary layer, pressure distribution, 設計最適化, compressibility effect, supersonic experimental airplane, attachment line contamination, natural laminar flow wing, supersonic aircraft

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::bf4c708cfc0bf1239910d4cf331df085Test
http://id.nii.ac.jp/1696/00005756Test/

المؤلفون: Misaka, Takashi, Obayashi, Shigeru

المصدر: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集 第37回・第38回 = JAXA Special Publication: Proceedings of the 37th and 38th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :31-34

مصطلحات موضوعية: 境界層遷移, RANSシミュレーション, turbulent reattachment, turbulent boundary layer, 計算流体力学, 乱流再付着, computational fluid dynamics, 速度分布, RANS simulation, 摩擦係数, Navier-Stokes equation, velocity distribution, 層流境界層, 層流剥離, laminar separation, 乱流境界層, friction coefficient, ナビエ・ストークス方程式, transition position, 渦度, laminar boundary layer, boundary layer transition, 遷移位置, vorticity

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::3a55a619e3ac6c65046a0205a5c86e41Test
http://id.nii.ac.jp/1696/00005923Test/

المؤلفون: Kobashi, Yasujiro, Hayakawa, Michio

المصدر: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集 第37回・第38回 = JAXA Special Publication: Proceedings of the 37th and 38th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :57-60

مصطلحات موضوعية: shear flow, せん断流, turbulent boundary layer, boundary layer, 境界層, 粘性, Physics::Fluid Dynamics, laminar flow, 層流境界層, Condensed Matter::Superconductivity, 乱流境界層, 渦度, vorticity model, laminar boundary layer, 渦度モデル, vorticity, turbulent flow, 渦度子, 数学モデル, 渦, vortex, 層流, 乱流, viscosity, 渦度束, vorticle, eddy, mathematical model

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::80c46d1a9626dfe68bd4699db5984ba3Test
http://id.nii.ac.jp/1696/00005930Test/

المؤلفون: Asai, Masahito, Konishi, Yasufumi

المصدر: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集 第37回・第38回 = JAXA Special Publication: Proceedings of the 37th and 38th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :21-24

مصطلحات موضوعية: 増幅, turbulent boundary layer, amplification, boundary layer, 境界層, 風洞試験, smokewire method, スモークワイヤ法, 層流境界層, 乱流境界層, particle image velocimetry, flow visualization, streak instability, laminar boundary layer, 流れの可視化, transient growth, 粒子画像速度計測法, ストリーク不安定, Sinuousモード, sinuous mode, 速度分布, velocity distribution, 渦, vortex, 過渡増幅, wind tunnel test

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::610a2ae40514c9691e0fbeaf867e2dddTest
http://id.nii.ac.jp/1696/00005920Test/

المؤلفون: Kohama, Yasuaki P., Kato, Takuma, Kikuchi, Satoshi, Ota, Fukuo

المصدر: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集 第33回・第34回 = JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :59-62

مصطلحات موضوعية: 境界層遷移, 流動環境シミュレータ, 地上効果, flow environment simulator, 風洞試験, 層流境界層, low speed wind tunnel, ground effect, research facility, flow visualization, 研究施設, wind tunnel test, laminar boundary layer, 低速風洞, boundary layer transition, 流れの可視化

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::20708cd3d5ac3bbd5429e94298921c8aTest
http://id.nii.ac.jp/1696/00006566Test/

المؤلفون: Ishii, Katsuya, Suzuki, Satoshi, Adachi, Shizuko

المصدر: 航空宇宙技術研究所特別資料: 境界層遷移の解明と制御研究会講演論文集 第29回・第30回 = Special Publication of National Aerospace Laboratory: Proceedings of the 29th and 30th NAL Workshops on Investigation and Control of Boundary-Layer Transition. 56:7-10

مصطلحات موضوعية: エーロフォイル, Mach number, vorticity distribution, 仰角, 音圧, angle of attack, 圧縮性Navier-Stokes方程式, separated flow, compressible Navier-Stokes equation, Reynolds number, research and development, Physics::Fluid Dynamics, 数値シミュレーション, 剥離流, 渦分布, 音響励起, 層流境界層, numerical simulation, Mach数, sound pressure, airfoil, laminar boundary layer, Reynolds数, 研究開発, acoustic excitation

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=jairo_______::a4278109a07d8729612f883c9bb1dfa7Test
http://id.nii.ac.jp/1696/00038188Test/