Výsledky vyhledávání - "遷音速風洞"

The cryogenic wind tunnel test on HOPE model

Autor: Niwa, Hiroaki, Saito, Katsuya, Nakano, Eiichiro, Aoki, Takeo, Yokomaku, Yoshio

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 42:111-131

21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)
HOPE-X(宇宙往還技術試験機)の実レイノルズ数付近における空力特性データを取得する為に、5%HOPE(H-2ロケット打ち上げ型有翼回収機)風洞試験模型を製

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b17f2640784f63369d3e4ecea1f08fd5
http://id.nii.ac.jp/1696/00037385/

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HYTEX pressure measurement test using pressure-sensitive paint at transonic and supersonic wind tunnels

Autor: Nakakita, Kazuyuki, Taguchi, Hideyuki, Ogawa, Tomotake, Nakatani, Hiroki, Ito, Masatake, Mitsuo, Kazunori, Kurita, Mitsuru

Publikováno v: 宇宙航空研究開発機構特別資料: 第79回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 79th Meeting. :27-32

JAXAで基礎研究を進めている極超音速実験機(HYTEX: HYpersonic Turbojet EXperiment)の遷音速および超音速での空力特性を確認するため、10％スケール模型を用いて1m×1m超音速風洞(SWT1: Supersonic Wind Tu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::08e8362e4b1d4db81e10cea887677d18
http://id.nii.ac.jp/1696/00005596/

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JAXA2m×2m遷音速風洞における測定部マッハ数検定試験

Autor: Kozai, Masataka, Ueno, Makoto, Shiohara, Tatsuro, Komatsu, Yukio, Karasawa, Toshio, Koike, Akira, Sudani, Norikazu, Ganaha, Yoshito, Kon, Naoki, Haraguchi, Tomohiro

Publikováno v: 宇宙航空研究開発機構特別資料: 第77回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 77th Meeting. :6-14

In the JAXA 2 m x 2 m Transonic Wind Tunnel, there have been more needs of wind tunnel users for high measurement accuracy to develop aircraft and launch vehicles with high performance. To achieve higher accuracy, more elaborate calibration tests to

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7e2eb969ae7aace556f02368728f4241
http://id.nii.ac.jp/1696/00005807/

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Stereoscopic PIV system applied to JAXA 2 m x 2 m Transonic Wind Tunnel

Autor: Kato, Hiroyuki, Watanabe, Shigeya, Karasawa, Toshio, Noguchi, Masayoshi, Hashimoto, Takuro, Yoshimura, Sadanori

Publikováno v: 宇宙航空研究開発機構特別資料: 第74回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 74th Meeting. :34-41

これまで主に低速風洞において整備を進めてきた可搬型PIVシステムに対して、遷音速風洞での適用を目的とした改良を加えた遷音速風洞用ステレオPIVシステムの開発を行った。計測シス�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0e9a70afe39214343f686e1c815b0e2f
http://id.nii.ac.jp/1696/00006171/

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On modernization of wind tunnels

Autor: Shigemi, Masashi, Sudani, Norikazu, Karasawa, Toshio

Publikováno v: 宇宙航空研究開発機構特別資料: 第73回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting. :33-38

すべての試験設備に言えることであるが、風洞は時間と共に老朽化、陳腐化する。これを防ぐためには、適切な時期に改修をすることが不可欠である。JAXA風洞技術開発センター(WINTEC)の�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a66ea602b9359f21180cb68e020b3d1a
http://id.nii.ac.jp/1696/00006423/

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Test for thermal performance evaluation of ESP scanner (PSI) with thermal compensation

Autor: Ito, Fumihiro, Hashimoto, Takeaki

Publikováno v: 宇宙航空研究開発機構特別資料: 第73回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting. :9-17

資料番号: AA0048471002
レポート番号: JAXA-SP-04-014

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::244cf9eb1d4d32b1410fe44c0a115146
http://id.nii.ac.jp/1696/00006420/

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Developments in measuring boundary-layer transition locations at WINTEC transonic wind-tunnels

Autor: Fujii, Keisuke, Sato, Mamoru, Noguchi, Masayoshi, Mitsuo, Kazunori, Hosoe, Nobuyuki

Publikováno v: 宇宙航空研究開発機構特別資料: 第72回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 72nd Meeting. :14-20

A series of wind tunnel tests were conducted to develop a boundary-layer tripping technique and also a detection technique for the boundary-layer state in transonic wind tunnels in ISTA/JAXA. A commonly used disk-type roughness element was used in th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fb3433f5673af583fec97f5a280a3a85
http://id.nii.ac.jp/1696/00006431/

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CFD code validation using pressure-sensitive paint measurement

Autor: Nakakita, Kazuyuki, Mitsuo, Kazunori, Kurita, Mitsuru, Watanabe, Shigeya, Yamamoto, Kazuomi, Mukai, Junichi, Takaki, Ryoji

Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004. :184-189

Pressure-Sensitive Paint (PSP) is an image base pressure measurement technique and its data has much larger pressure information than the conventional pressure tap measurement. It produces quantitative pressure data. The PSP was estimated its perform

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6c161526049c466aa11e570ef4bc9d9a
http://id.nii.ac.jp/1696/00006465/

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Quantitative measurement of unsteady pressure field on a delta wing by means of a fast-response PSP

Autor: Tabei, Takatoshi, Kawakami, Takaho, Kameda, Masaharu, Nakakita, Kazuyuki

Publikováno v: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :128-131

資料番号: AA0048089033

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2c00d1b72debf7ccf8d40e80d5dc5577
http://id.nii.ac.jp/1696/00014634/

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PSP test using ONERA M5 standard model at JAXA 2 m x 2 m transonic wind tunnel

Autor: Nakakita, Kazuyuki, Kurita, Mitsuru, Mitsuo, Kazunori, Koike, Akira, Watanabe, Shigeya, Ito, Masatake, Hashimoto, Takuro

Publikováno v: 宇宙航空研究開発機構特別資料: 第71回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 71st Meeting. :46-51

風洞技術開発センター(以下WINTEC)では大型実用風洞で感圧塗料(Pressure-sensitive paint;以下PSP)試験を行うための実用PSP計測システムを整備中である。PSPの特徴を簡単に述べるとともに、実用PS

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2f2a1017c3162720aa810eb5a223905c
http://id.nii.ac.jp/1696/00006485/

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