Zobrazeno 1 - 10
of 26
pro vyhledávání: '"combustion vibration"'
Autor:
Taghizadeh-Alisaraei, Ahmad1 ahmadtza@yahoo.com, Rezaei-Asl, Abbas1
Publikováno v:
Fuel. Dec2016, Vol. 185, p718-733. 16p.
Autor:
Taghizadeh-Alisaraei, Ahmad1 Ahmadtza@yahoo.com, Ghobadian, Barat2 Ghobadib@modares.ac.ir, Tavakoli-Hashjin, Teymour2 Ttavakol@modares.ac.ir, Mohtasebi, Seyyed Saeid3 mohtaseb@ut.ac.ir, Rezaei-asl, Abbas1 arezaeiasl@yahoo.com, Azadbakht, Mohsen1 azadbakht39@yahoo.com
Publikováno v:
Renewable Energy: An International Journal. Sep2016, Vol. 95, p422-432. 11p.
Publikováno v:
International Journal of Automotive Technology; Feb2019, Vol. 20 Issue 1, p187-195, 9p
Publikováno v:
Journal of Insect Behavior; Nov2018, Vol. 31 Issue 6, p599-615, 17p
Publikováno v:
Journal of Low Frequency Noise, Vibration & Active Control; Jun2015, Vol. 34 Issue 2, p107-118, 11p
Autor:
Allouis, C.1 allouis@irc.cnr.it, Amoresano, A.2, Capasso, R.2, Langella, G.2, Niola, V.2, Quaremba, G.2
Publikováno v:
Fuel Processing Technology. Oct2018, Vol. 179, p10-16. 7p.
Publikováno v:
宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :201-206
An active control of combustion driven oscillations occurring in a lean premixed model combustor is demonstrated by means of a secondary fuel injection. An unstable condition, which leads to self-excited pressure oscillations beyond 170 dB, is chosen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::d85d6dc9d8084f9c9290624e58923cc6
http://id.nii.ac.jp/1696/00006022/
http://id.nii.ac.jp/1696/00006022/
Publikováno v:
宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems. :93-98
The system firing test for HTV (H-2 Transfer Vehicle) was performed on June thru August, 2004. The result shows that the system provides approximately 50 percent thrust during short impulse RCS firings using four forward thrusters with GHe saturated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::ff532a8857bddd3f5f350041748c143d
http://id.nii.ac.jp/1696/00006244/
http://id.nii.ac.jp/1696/00006244/
Publikováno v:
宇宙輸送シンポジウム 平成14年度 = Proceedings of Space Transportation Symposium FY2002. :103-106
資料番号: AA0045426026
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::28575812ed0d2e3f483582d97cb33b89
http://id.nii.ac.jp/1696/00017356/
http://id.nii.ac.jp/1696/00017356/
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