多列円板を有する伸展式エアロスパイクの空力特性

• 小林 弘明

  宇宙航空研究開発機構

• 丸 祐介

  日本学術振興会特別研究員PD（東京大学大学院工学系研究科）

• 佐藤 哲也

  宇宙航空研究開発機構

書誌事項

タイトル別名

• Aerodynamic Characteristics of Telescopic Aerospikes with Multiple-Row-Disk
• タレツ エンバン オ ユウスル シンテンシキ エアロスパイク ノ クウリキ トクセイ

抄録

This paper reports experimental studies on telescopic aerospikes with multiple disks. The telescopic aerospike is useful as an aerodynamic control device; however, changing its length causes a buzz phenomenon, which many researchers have reported. The occurrence of buzzing might be critical to the vehicle because it brings about severe pressure oscillations on the surface. Disks on the shaft produce stable recirculation regions by dividing the single separation flow into several conical cavity flows. The telescopic aerospikes with stabilizer disks are useful without any length constraints. Aerodynamic characteristics of the telescopic aerospikes were investigated through a series of wind tunnel tests. Transition of recirculation/reattachment flow modes of a plain spike causes a large change in the drag coefficient. Because of this hysteresis phenomenon and the buzzing, the plain spike is unsuitable for fine aerodynamic control devices. Adding stabilizer disks is effective for the improved control of aerospikes.

収録刊行物

• 日本航空宇宙学会論文集

  日本航空宇宙学会論文集 55 (642), 329-336, 2007

  一般社団法人 日本航空宇宙学会

キーワード

• Aerodynamic Characteristics
• Aerospikes
• Rockets
• Missiles
• Unsteady Flows

詳細情報

• CRID: 1390282679447442304
• NII論文ID: 10019783909
• NII書誌ID: AA11307372
• DOI: 10.2322/jjsass.55.329
• ISSN: 24323691
• ISSN: 13446460
• NDL書誌ID: 8893949
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I8893949
• Web Site: https://www.jstage.jst.go.jp/article/jjsass/55/642/55_642_329/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
  • KAKEN
• 抄録ライセンスフラグ: 使用不可