WEKO3
アイテム
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2台のAGARD-B標準模型による並列二段式往還機の超音速空力特性試験
https://jaxa.repo.nii.ac.jp/records/39758
https://jaxa.repo.nii.ac.jp/records/39758e8304be8-ff6a-48c4-8d20-d2252c9f6250
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltm00692.pdf (10.7 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 2台のAGARD-B標準模型による並列二段式往還機の超音速空力特性試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2段式往還機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | AGARD-B標準模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行領域 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 6分力天秤 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 迎角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 相互作用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 操縦性能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 抗力 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two stage to orbit vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | AGARD B standard model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cruising region | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic interference | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | six force balance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic force | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | maneuverability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | drag | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Aerodynamic characteristics of parallel two-stage-to-orbit vehicles using two AGRAD-B standard models in supersonic flows | |||||
著者 |
野田, 順一
× 野田, 順一× 石田, 清道× 関根, 英夫× 原, 亘利× 榊原, 盛三× 河本, 巖× Noda, Junichi× Ishida, Kiyomichi× Sekine, Hideo× Hara, Nobutoshi× Sakakibara, Seizo× Kawamoto, Iwao |
|||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 692, p. 1-36, 発行日 1996-04 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 並列2段式往還機(TSTO)の超音速領域での飛行と分離を想定して、空力特性がよく知られているAGARD-B模型とその1/2縮尺模型を並行に配置し、2台の模型の迎角と模型間の距離およびマッハ数を変えて空力干渉の試験を行った。各々の模型に組み込まれた6分力天秤で空気力を測定し、単独模型の場合の空力特性と比較した。第1段・第2段模型相互による空力的な干渉の結果、マッハ数・迎角・模型間の距離(垂直および前後方向)によって空力特性(揚力係数および縦揺れモーメント係数)が大きく変化する。従って、第2段機が分離するときに高度の操縦性能が要求される。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To obtain the aerodynamic characteristics of the interaction of parallel Two-Stage-To-Orbit (TSTO) space vehicles in the cruising regions and separation in the supersonic flow, in the range of M(sub infinite) that is equal to or between 1.5 and 2.5, an AGARD (Advisory Group for Aerospace Research and Development)-B standard model and its half-model were tested using two six force balances. By arranging the two models parallel in the same direction and changing the distance and the angle of attack in the range where alpha is greater than or equal to -12 and less than or equal to 12 deg, six aerodynamic force coefficients were measured and compared with the coefficients for a single model. The aerodynamic forces of the upper second stage plane model varied a short distance behind the shock waves of the partner plane. This indicates that sturdy maneuverability is required for a TSTO, especially for the upper second plane during their separation process. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000441000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-692 |