Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Fumiya Tsutsui"'
Publikováno v:
Journal of Spacecraft & Rockets. Mar2024, Vol. 61 Issue 2, p355-368. 14p.
Publikováno v:
Journal of Spacecraft and Rockets. 59:1697-1712
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e2004b5f56450b4a17ac30c9753c255
https://doi.org/10.2514/1.a35319
https://doi.org/10.2514/1.a35319
Publikováno v:
Journal of Spacecraft and Rockets. 59:225-235
This paper presents the experimental and analytical results of a heat rejection system consisting of a single-phase mechanically pumped loop and a space radiator. It has been developed for future c...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::59c7894e08cd4c5412c9383cd4916b8f
https://doi.org/10.2514/1.a35030
https://doi.org/10.2514/1.a35030
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cba8635662cb2b6eec9776c46e1907c1
https://doi.org/10.2514/6.2023-0241
https://doi.org/10.2514/6.2023-0241
Publikováno v:
International Journal of Aeronautical and Space Sciences.
A slender-bodied vehicle with asymmetrically arranged protuberance generates strong side force due to asymmetric vortices, even at a low angle-of-attack. We investigated effects of the well-known RANS turbulence models [SA-R (Crot = 0.0, 1.0, and 2.0
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f2a14181a368d063486e33fd64637825
http://hdl.handle.net/10131/00014761
http://hdl.handle.net/10131/00014761
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::16330c01067a86dc5d7a93f6a195d47e
https://doi.org/10.2514/6.2021-0137
https://doi.org/10.2514/6.2021-0137
Publikováno v:
The proceedings of the JSME annual meeting. :543-544
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd88afc4f2fd486e943da63edf5f67a4
https://doi.org/10.1299/jsmemecjo.2000.4.0_543
https://doi.org/10.1299/jsmemecjo.2000.4.0_543
Publikováno v:
Journal of Spacecraft & Rockets. Jan2022, Vol. 59 Issue 1, p225-235. 11p.