JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
61881000.pdf4.5 MB
title超音速流中に置かれた軸対称物体の表面静圧変動
Other TitleSurface pressure fluctuation on axisymmetric bodies in supersonic flows
Author(jpn)徳川, 直子
Author(eng)Tokugawa, Naoko
Author Affiliation(jpn)宇宙航空研究開発機構航空プログラムグループ超音速機チーム(JAXA)(APG)
Author Affiliation(eng)Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)(APG)
Issue Date2013-03-29
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発資料
JAXA research and development memorandum
VolumeJAXA-RM-12-011
Start page1
End page31
Publication date2013-03-29
Languagejpn
eng
Abstract境界層の遷移機構を正しく理解した上で遷移位置を予測する精度をより高めていくために,超音速流中に置かれた軸対称物体を対象として2003年3月から2012年12月に著者らが実施した試験結果のうち,表面静圧変動計測に関する結果をまとめる.
Experimental results of surface pressure measurements on axisymmetric bodies in supersonic flows, which were obtained from 2003 to 2012, are summarized. It aims to improve numerical technique to predict laminar-turbulent transition in boundary layer with understanding of transition mechanism.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Keywordssurface pressure fluctuation; supersonic; boundary layer transition; experiment
Document TypeTechnical Report
JAXA Category研究開発資料
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0061881000
Report NoJAXA-RM-12-011
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/15815


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