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規格・テクニカルリポート類

遷音速後退翼に対する境界層効果の評価

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遷音速後退翼に対する境界層効果の評価

Material type
規格・テクニカルリポート類
Author
小松, 浩司ほか
Publisher
航空宇宙技術研究所
Publication date
1984-11
Material Format
Digital
Capacity, size, etc.
-
NDC
-
View Details

Notes on use

Note (General):

出版タイプ: NAA comparison of the result of numerical analysis with experimental data is made for the ONERA M-6 and the practical transonic wing model 7202...

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
小松, 浩司
飯田, 栄治
河村, 龍馬
廣瀬, 直喜
松野, 謙一
Komatsu, Koji
Iida, Eiji
Kawamura, Ryuma
Hirose, Naoki
Matsuno, Ken-ichi
Publication, Distribution, etc.
Publication Date
1984-11
Publication Date (W3CDTF)
1984-11
Alternative Title
The Analysis of Practical Transonic Swept Wings with and without Boundary Layer Effects
Periodical title
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-3
No. or year of volume/issue
3
Volume
3
Pages
305-312
ISSN (Periodical Title)
ISSN : 0289-260X
Text Language Code
jpn
Target Audience
一般
Note (General)
出版タイプ: NA
A comparison of the result of numerical analysis with experimental data is made for the ONERA M-6 and the practical transonic wing model 720211. The Jameson-Caughey's transonic wing programs FLO22 and FLO27 are used. The wing aerodynamic characteristics with viscous effect are evaluated by taking into account the boundary layer friction drag. This drag is calculated by using a three-dimensional compressible boundary layer program for wings, BLAY. Finally, a viscous-inviscid interaction procedure for FLO27-BLAY is proposed, and a preliminary result is presented.
資料番号: NALSP0003035
レポート番号: NAL SP-3
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)
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