{"created":"2023-06-20T14:37:48.249303+00:00","id":4241,"links":{},"metadata":{"_buckets":{"deposit":"b4045ba3-303d-4d06-b1a5-50c87f72e17c"},"_deposit":{"created_by":1,"id":"4241","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4241"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004241","sets":["1398:1530:1537","1543:1874:1881","1887:1891","9:789:888:896"]},"author_link":["18513","18517","18514","18512","18516","18515"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Validation of Measurement Accuracy for Near-Field Pressure of Supersonic Projectiles Using a Ballistic Range"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-12-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper reports the results of near-field pressure measurement tests to validate the measurement accuracy in a ballistic range at the Institute of Fluid Science, Tohoku University. The experiments in the ballistic range were performed using two types of axisymmetric projectile which have sharp and blunt nose shape, respectively. The near-field pressure waveforms measured in this experiment were compared to the existing results obtained in the wind tunnel experiments using a static pressure probe. Since the sting support influences were shown in the wind tunnel experimental data, only the front part of the waveform could be compared. The results showed that the nearfield pressure waveform of the sharp nose projectile qualitatively agreed with the existing experimental data although the measurement conditions such as angle-of-attack and Mach number in the ballistic range experiment differed from those in the wind tunnel. On the other hand, the blunt nose projectile comparatively flew horizontally and its measured near-field pressure waveform quantitatively agreed well with the existing experimental data. It was confirmed by a numerical simulation that the small difference of the flight conditions did not have a large influence on the near-field pressure value. These experiment results indicate that this ballistic range has an ability to measure near-field pressure waveform correctly.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061958001","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-12-010","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_value":"東北大学流体科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鵜飼, 孝博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大谷, 清伸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大林, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ukai, Takahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ohtani, Kiyonobu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obayashi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-16"}],"displaytype":"detail","filename":"61958001.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61958001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4241/files/61958001.pdf"},"version_id":"9da06b43-df6f-44f5-b4d6-51f5c7a60a7b"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"弾道飛行装置を用いた超音速飛行体の近傍場圧力計測精度の検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"弾道飛行装置を用いた超音速飛行体の近傍場圧力計測精度の検証"}]},"item_type_id":"5","owner":"1","path":["896","1537","1881","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4241","relation_version_is_last":true,"title":["弾道飛行装置を用いた超音速飛行体の近傍場圧力計測精度の検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:44:09.981127+00:00"}