Systems and Methods for Aerial and Ground-Based
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- NAKA Yusuke
- Aircraft Systems Research Group, Institute of Aeronautical Technology
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- SHINDO Shigemi
- Technology Demonstration Research Office Mission Planning Group, Institute of Aeronautical Technology
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- MAKINO Yoshikazu
- Aircraft Systems Research Group, Institute of Aeronautical Technology
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- KAWAKAMI Hiroki
- Aircraft Systems Research Group, Institute of Aeronautical Technology
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抄録
For validating"low-boom"supersonic aircraft design concepts and techniques in flight tests, sonic booms must be measured accurately. This paper discusses the systems and methods for accurate sonic boom measurement both on and above the ground. Requirements and issues for sonic boom measurement systems are considered and possible solutions are shown with the measurement systems and methods the authors have developed as examples. For the aerial measurement, the system and method for recording sonic booms at multiple altitudes up to about 1000 m above the ground by using a tethered blimp have been developed. The sonic boom data measured in the recent flight tests demonstrated the validity of the systems and methods for aerial and ground-based sonic boom measurement.
収録刊行物
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- 宇宙航空研究開発機構研究開発報告
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宇宙航空研究開発機構研究開発報告 13 1-19, 2013-10
宇宙航空研究開発機構
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詳細情報 詳細情報について
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- CRID
- 1572261552815602816
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- NII論文ID
- 110009660087
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- NII書誌ID
- AA1192675X
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- ISSN
- 13491113
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- 本文言語コード
- en
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- データソース種別
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- CiNii Articles