@inproceedings{oai:jaxa.repo.nii.ac.jp:00037182,
 author = {航空宇宙技術研究所 and National Aerospace Laboratory},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {22-23 May 1997 (58th). 27-28 Nov. 1997 (59th), 22-23 May 1997 (58th). 27-28 Nov. 1997 (59th), 本論文集では、以下の風洞研究について論じた。大型高温衝撃風洞(HIEST)の設計と空力試験、超音速風洞および遷音速風洞のデータ処理設備、2次元風洞の改修、アーク加熱気流の計測、高仰角試験、感圧塗料のサンプル特性試験、低速および遷音速風洞試験、ALFLEX(小型自動着陸実験)実験機空力データベース、飛行速度ベクトル計測システムの特性と装置、高速多点圧力計測装置、風洞計測システム、およびHOPE(H-2ロケット打上げ型有翼回収機)におけるピッチングモードフラッタ。, The following researches on wind tunnel are discussed: design and aerodynamic tests of High Enthalpy Shock Tunnel (HIEST), data processing equipment of both supersonic and transonic wind tunnels, improvement of two-dimensional wind tunnel, measurements of an arc heated flow, high angle of attack test, sample tests of pressure-sensitive paints, wind tunnel test of both low-speed and transonic flows, ALFLEX aerodynamic database, characteristic and equipment of air data system, high-speed pressure acquisition system, wind tunnel instrumentation system, and pitching mode flutter for HOPE (H-2 Orbiting Plane)., 資料番号: AA0001434000, レポート番号: NAL SP-38},
 pages = {1--232},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {第58回・第59回風洞研究会議論文集},
 volume = {38},
 year = {1998}
}