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超音速航空機(SST)形態の高揚力装置に関する実験的研究

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宮田, 勝弘, 李家, 賢一, Kwak, Dong-Youn, 野口, 正芳, Miyata, Katsuhiro, Rinoie, Kenichi, Noguchi, Masayoshi航空宇宙技術研究所2003-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1456

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Subject Heading...d leading edge high lift device wing surface pressure ...
Alternative Title...estigations on high lift devices for an SST
Alternative Title...estigations on high lift devices for an SST

Progress in boundary-layer transition prediction

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Malik, Mujeeb R.航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory48Tp.67-70

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Subject Heading...imization code high lift transition prediction crossfl...

低騒音STOL実験機機体開発総合報告書

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STOLプロジェクト推進本部機体技術開発室, Aircraft, D. S. STOL Aircraft Proj. G.航空宇宙技術研究所1994-01航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1223p.1-135

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Subject Heading...earch aircraft high lift device USB system fan jet eng...

低騒音STOL実験機「飛鳥」の水平尾翼付近の流れ計測

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STOLプロジェクト推進本部, STOL Research Aircraft Group航空宇宙技術研究所1993-06航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1207p.1-17

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Subject Heading...sh measurement high lift device powered lift system ST...
Note (General)... aircraft with high lift. Flow characteristics such as...

Experimental studies of vortex flaps and vortex plates, Part 2: 1.15m span 60 deg delta wing

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李家, 賢一, Stollery, L., Rinoie, Kenichi, Stolley, L.航空宇宙技術研究所1992-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1180Tp.1-36

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Subject Heading...ow measurement high lift take off and climb performanc...

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