Zobrazeno 1 - 10
of 65
pro vyhledávání: '"Yousuke Ogino"'
Publikováno v:
JOURNAL OF THE JAPAN WELDING SOCIETY. 92:5-5
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::179a80dca7b5ffb9be3630e4c7204e51
https://doi.org/10.2207/jjws.92.5
https://doi.org/10.2207/jjws.92.5
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cec40001ce44e15dce5bf3f332cec5a
https://doi.org/10.2514/6.2021-0208
https://doi.org/10.2514/6.2021-0208
Publikováno v:
Journal of Spacecraft and Rockets. 54:191-198
This paper explores a suitable position for a dust-capturing device on the surface of an aeroflyby hypersonic vehicle traveling in the Martian atmosphere at an altitude of 36 km. The feasibility of the Mars aeroflyby sample collection as a mission fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efe8ff1e7eec53d195e8f122681fbc4d
https://doi.org/10.2514/1.a33439
https://doi.org/10.2514/1.a33439
Publikováno v:
The Proceedings of Conference of Chugoku-Shikoku Branch. :07b4
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::753f5906f8b5e32579f13e1fd13d87f6
https://doi.org/10.1299/jsmecs.2021.59.07b4
https://doi.org/10.1299/jsmecs.2021.59.07b4
Publikováno v:
Aerospace Science and Technology. 50:256-265
A cause of an overestimation of the computed surface pressure on a blunted cone in high-temperature hypersonic flow is explored. The overestimation was observed in a free-piston shock tunnel at the stagnation of H 0 = 15.6 and 10.1 MJ/kg. The sensiti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4668219ffa70c1bea2ca1b8fb043566
https://doi.org/10.1016/j.ast.2015.12.015
https://doi.org/10.1016/j.ast.2015.12.015
Publikováno v:
Journal of Spacecraft and Rockets. 52:375-382
An appropriate position of dust capturing device on the surface of aero-flyby capsule flying at a velocity of 4.4 km/s in Martian atmosphere at an altitude of 36 km is explored. The equation of motion and heat transfer equation for dust particles are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1ed431cc8cf7188c4a707e23fbd063d
https://doi.org/10.2514/1.a32827
https://doi.org/10.2514/1.a32827
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 58:319-326
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd51a6c24d00a5de0a1cfbcd14093f70
https://doi.org/10.2322/tjsass.58.319
https://doi.org/10.2322/tjsass.58.319
Publikováno v:
Mathematical Problems in Engineering. 2014, p1-20. 20p.
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b560aedfac2a830e6b55777a90b683ed
https://doi.org/10.2514/6.2017-1695
https://doi.org/10.2514/6.2017-1695
Publikováno v:
Open Journal of Fluid Dynamics. :321-333
A supersonic turbulent flowfield involving the pseudo-shock waves in an isolator of a supersonic combustion ramjet is computed using two different LES codes which are a high-order upwind finite volume scheme, and a sixth order compact differencing sc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73d55983ce26d286dfa94a34f49a9d9b
https://doi.org/10.4236/ojfd.2014.43024
https://doi.org/10.4236/ojfd.2014.43024