Zobrazeno 1 - 10
of 23
pro vyhledávání: '"six component balance"'
Publikováno v:
Polish Maritime Research, Vol 27, Iss 3, Pp 4-15 (2020)
In order to obtain the hydrodynamic coefficients that can save cost and meet the accuracy requirements, a new hydrodynamic test platform based on a 6DoF (six degrees of freedom) parallel mechanism is proposed in this paper. The test platform can driv
Externí odkaz:
https://doaj.org/article/fbb1771bcb954f93b74f6a85769e9d23
Publikováno v:
Polish Maritime Research, Vol 27, Iss 3, Pp 4-15 (2020)
In order to obtain the hydrodynamic coefficients that can save cost and meet the accuracy requirements, a new hydrodynamic test platform based on a 6DoF (six degrees of freedom) parallel mechanism is proposed in this paper. The test platform can driv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7bd10baf3fc81a76aca6194c4d1ec39d
https://doi.org/10.2478/pomr-2020-0041
https://doi.org/10.2478/pomr-2020-0041
Autor:
Zedník, Roman
This master thesis focuses on designing of an external six-component balance. This universal concept would provide access of results from different models of wings, aircraft and automobiles with relatively small scales. This work also includes theore
Externí odkaz:
http://www.nusl.cz/ntk/nusl-417795
Autor:
Wemans, Miguel
O túnel aerodinâmico da Academia da Força Aérea é uma infra-estrutura única a nível nacional, que permite a simulação de escoamentos em torno de modelos para validação de análise aerodinâmica e de estabilidade. De forma a tirar partido d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1714::738f025c28ba90573052cdc9901285cc
https://hdl.handle.net/10400.26/39772
https://hdl.handle.net/10400.26/39772
Akademický článek
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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
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/
http://id.nii.ac.jp/1696/00037385/
Autor:
Shirai, Masataka, Hozumi, Koki
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 42:137-140
21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)
航空宇宙技術研究所の所有する実験用航空機、ドルニエ式Do-228-200型機をインフライト・シミュレータ、多目的実証実験機MuPAL(Multi-Purpose Aviation Laborat
航空宇宙技術研究所の所有する実験用航空機、ドルニエ式Do-228-200型機をインフライト・シミュレータ、多目的実証実験機MuPAL(Multi-Purpose Aviation Laborat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::6181b6101a913cdf0daac40b1c77e716
http://id.nii.ac.jp/1696/00037387/
http://id.nii.ac.jp/1696/00037387/
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 690:1-48
航技研の遷音速風洞(NAL-TWT)に設置してある内挿式6分力天秤用較正装置は成分荷重方式であり、最初の一体化天秤の較正に必要な複合荷重機能が欠けていた。この機能不足を補うために199
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::30dd670f773b3b71f39a67bb09e31fb8
http://id.nii.ac.jp/1696/00039785/
http://id.nii.ac.jp/1696/00039785/
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
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Autor:
Rawlings, B.
This report provides an overview of the underwater vehicle six-component balance (dyno) and the procedure used to calibrate it in Nov/Dec 2002, along with the calibration results. There is then an overview of the Victoria class submarine model, and t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1674::ce966ae8e78465448fd973426b5611f8
https://nrc-publications.canada.ca/eng/view/object/?id=e619a8b6-7515-4e4f-96df-519a1394a379
https://nrc-publications.canada.ca/eng/view/object/?id=e619a8b6-7515-4e4f-96df-519a1394a379