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航空機の動揺のり心地に関する一実験
https://jaxa.repo.nii.ac.jp/records/44739
https://jaxa.repo.nii.ac.jp/records/44739b4490426-44dd-426f-bd55-4735318fcee5
名前 / ファイル | ライセンス | アクション |
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naltr00486.pdf (904.5 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航空機の動揺のり心地に関する一実験 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | An Experimental Investigation of the Riding Qualities of Aircraft | |||||
著者 |
幸尾, 治朗
× 幸尾, 治朗× 斎藤, 秀夫× 矢沢, 健司× 塚野, 雄吉× 小野, 孝次× KOO, Jiro× SAITO, Hideo× YAZAWA, Kenji× TSUKANO, Yukichi× ONO, Takatsugu |
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著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-486 巻 486, p. 11, 発行日 1977-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Recently, it has been claimed that motion sickness is due to confusion created in the central nervous system of the brain by conflicting position and motion informations arriving from visual and vestibular organs. This is one of the series of experimental studies designed to determine what are the physiological and psychological causes of motion sickness. Using a “variable stability aircraft”as a wave like heaving motion accelerator, in-flight experiments were carried out to introduce a psychological comfort characteristic curve which relates to riding qualities and motion period.“Method of Pair Comparisons”in the field of psychology were adopted to analyze the experimental data. It was found that the discomfort peak appeared near the 5 second heaving motion period. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0486000 | |||||
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 TR-486 |