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CASPERによるF-16A戦闘機のCFD計算とその検証
https://jaxa.repo.nii.ac.jp/records/37491
https://jaxa.repo.nii.ac.jp/records/37491a3ea183a-0109-462f-9307-b9dfb7041dbc
名前 / ファイル | ライセンス | アクション |
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nalsp0044058.pdf (683.5 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | CASPERによるF-16A戦闘機のCFD計算とその検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CASPER | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算空気力学システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | F-16A戦闘機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ場 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非構造格子 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CASPER | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational aerodynamic system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | F 16A aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow field | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structured grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unstructured grid | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | CFD computation and validation of an F-16A aircraft configuration using the CASPER | |||||
著者 |
沖, 良篤
× 沖, 良篤× 酒田, 威志× 海田, 武司× 惠上, 浩一× 谷, 泰寛× Oki, Yoshiatsu× Sakata, Takeshi× Kaiden, Takeshi× Egami, Koichi× Tani, Yasuhiro |
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著者所属 | ||||||
防衛庁 技術研究本部 | ||||||
著者所属 | ||||||
防衛庁 技術研究本部 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Defense Agency Technical Research and Development Institute | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Defense Agency Technical Research and Development Institute | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 44, p. 363-368, 発行日 1999-12 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 16-18 Jun. 1999 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 16-18 Jun. 1999 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本報は、防衛庁技術研究本部において開発されてきたCASPER(性能評価と研究のための計算空気力学システム)の成果を提示している。CASPERは種々の先進航空機の空力設計のためのCFD(数値流体力学)ベースの設計システムである。現在のCFDコードは構造格子および非構造格子を用いる3次元オイラー解析ソルバで構成されている。コードを検証するために、F-16A戦闘機形態周りの遷音速(一様流マッハ数M(sub ∞)=0.9)および超音速(M(sub ∞)=1.2))の流れ場を計算した。揚力、抗力、縦揺れモーメントおよび圧力係数について、計算結果と風洞実験による結果との良い一致を得た。航空機全機形態の空力設計に、CASPERが非常に強力なツールであることが明らかになった。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper shows the results of the CASPER (Computational Aerodynamics System for Performance Evaluation and Research) that has been developed in Technical Research and Development Institute of Japan Defense Agency. The CASPER is a CFD (Computational Fluid Dynamics)-based design system for the aerodynamic design of various advanced aircraft. The present CFD code consists of three-dimensional Euler analysis solver using structured and unstructured grids. In order to verify the code, transonic (free-stream Mach number M(sub infinity) = 0.9) and supersonic (M(sub infinity) = 1.2) flow fields around an F-16A aircraft configuration were computed. The computational results of lift, drag, pitching moment and pressure coefficients are in a good agreement with those of wind-tunnel experiments. It becomes clear that the CASPER is a very powerful tool for aerodynamic design of complete aircraft configurations. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001961058 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-44 |