Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Kenji Tadakuma"'
Nowadays the automotive industry is facing big threats from rapidly evolving technologies such as Artificial Intelligence, Big Data, connected technologies, clean energy demands for renewable energy and electric vehicles. Furthermore, business expect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e7fc8f32a81d9c315384d163253c9f04
https://doi.org/10.4337/9781789909814.00012
https://doi.org/10.4337/9781789909814.00012
Autor:
Kazuhiro Maeda, Takashi Sugiyama, Kentaro Tsuboi, Masashi Iyota, Kenji Tadakuma, Takafumi Makihara, Sadato Sugiyama, Kazuyoshi Kosaka, Susumu Terakado
Publikováno v:
SAE International Journal of Passenger Cars - Mechanical Systems. 10:309-317
Publikováno v:
SAE International Journal of Passenger Cars - Mechanical Systems. 10:358-368
Publikováno v:
SAE International Journal of Passenger Cars - Mechanical Systems. 9:645-656
Publikováno v:
Open Journal of Fluid Dynamics. :222-233
An experimental study on examining aerodynamic characteristics of fuselage cross sections for RLVs (Reusable Launch Vehicles) was conducted at Mach number 0.3, 0.9 and 4.0 in the wind tunnel of ISAS (Institute of Space and Astronautical Science), JAX
Autor:
Kenji Tadakuma
Publikováno v:
Open Journal of Fluid Dynamics. :234-241
Short Retraction Notice The paper does not meet the standards of "Open Journal of Fluid Dynamics". This article has been retracted to straighten the academic record. In making this decision the Editorial Board follows COPE's Retraction Guidelines. Ai
Autor:
Kenji Tadakuma
Publikováno v:
Open Journal of Fluid Dynamics. :263-271
Short Retraction Notice The paper does not meet the standards of "Open Journal of Fluid Dynamics". This article has been retracted to straighten the academic record. In making this decision the Editorial Board follows COPE's Retraction Guidelines. Ai
Autor:
Kazuhiro Maeda, Takashi Sugiyama, Masahiro Ohta, Masashi Iyota, Yoshinao Komatsu, Kenji Tadakuma
Publikováno v:
SAE International Journal of Passenger Cars - Mechanical Systems. 7:603-616
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 55:288-292
An experimental study on aerodynamic effect of RLVs (Reusable Launch Vehicles) due to fuselage cross sections has been conducted in subsonic flow. Three fuselage models and two wing-body models have been considered. Fuselage models have a circular, a
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 55:282-287