超音速境界層の振動マッハ波に対する受容性

Material type: 文書・図像類

Author: 坂上, 昇史ほか

Publisher: 航空宇宙技術研究所

Publication date: 2003-06

Material Format: Digital

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Note (General)：: The present paper describes our numerical study of supersonic boundary layer receptivity to oscillating Mach waves incident onto leading edge at a fre...

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Material Type: 文書・図像類
Title: 超音速境界層の振動マッハ波に対する受容性
Author/Editor: 坂上, 昇史
西岡, 通男
SAKAUE, Shoji
NISHIOKA, Michio
Author Heading: 坂上, 昇史
西岡, 通男
SAKAUE, Shoji
NISHIOKA, Michio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 2003-06
Publication Date (W3CDTF): 2003-06
Alternative Title: On the Receptivity of Supersonic Boundary Layer to Oscillating Mach Waves
Periodical title: 独立行政法人航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-59
No. or year of volume/issue: 59
Volume: 59
Pages: 4-
ISSN (Periodical Title): ISSN : 1347-457X
Text Language Code: jpn
Subject Heading: Supersonic Boundary Layer, Receptivity, Oscillating Mach Wave, Stokes Layer
Target Audience: 一般
Note (General): The present paper describes our numerical study of supersonic boundary layer receptivity to oscillating Mach waves incident onto leading edge at a freestream Mach number 2.2. We examine the external disturbance field around the leading edge in detail to clarify the formation of oscillating Stokes layer and its evolution into TS wave.
資料番号: NALSP0059009
レポート番号: NAL SP-59
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ