Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Wataru Sarae"'
Autor:
Hajime Okamoto, Wataru Sarae, Nobuo Sugimoto, Tomoaki Nishizawa, Kaori Sato, Akito Hattori, Atsushi Sawada, Yoshihiro Yamasaki, Yoshitaka Jin, Taisuke Yoshitomi
Publikováno v:
Applied Optics. 58(23):6274-6279
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2019-07-08
資料番号: PA1910042000
Physical characteristics: Original contains color illustrations
Accepted: 2019-07-08
資料番号: PA1910042000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3262fbf616c11b6fbb01b96673cdf7d5
http://id.nii.ac.jp/1696/00023019/
http://id.nii.ac.jp/1696/00023019/
Autor:
Wataru Sarae, Takehiro Himeno, Yutaka Umemura, Tetsuya Sato, Kiyoshi Kinefuchi, Hiroaki Kobayashi, Takeshi Fujita, Satoshi Nonaka, Koichi Okita
Publikováno v:
Journal of Spacecraft and Rockets. 56(1):91-103
Accepted: 2018-05-21
資料番号: SA1180213000
資料番号: SA1180213000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1fa293f46a94b3f248e3803d16145034
http://id.nii.ac.jp/1696/00029984/
http://id.nii.ac.jp/1696/00029984/
Publikováno v:
Journal of Spacecraft and Rockets. 55(6):1537-1544
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2018-04-20
資料番号: PA1910058000
Physical characteristics: Original contains color illustrations
Accepted: 2018-04-20
資料番号: PA1910058000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b166221a04b3420c8e7c92179eb4f8e3
http://id.nii.ac.jp/1696/00023035/
http://id.nii.ac.jp/1696/00023035/
Autor:
Kiyoshi Kinefuchi, Osamu Kawanami, Yutaka Umemura, Wataru Sarae, Hiroaki Kobayashi, Takehiro Himeno
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::685e80ca00ab9b50ff9f4db704e2f657
https://doi.org/10.2514/6.2017-4761
https://doi.org/10.2514/6.2017-4761
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d81aed5286fcbe7a074ed3cbc53f4a3
https://doi.org/10.2514/6.2017-3211
https://doi.org/10.2514/6.2017-3211
Autor:
Wataru Sarae, Hiroaki Kobayashi, Masao Takegoshi, Ayano Mori, Keita Terashima, Seiji Tsutsumi
Publikováno v:
The Journal of the Acoustical Society of America. 146:3001-3001
H3-scaled Acoustic Reduction Experiments (HARE) with a scale of 2.5 % was conducted for the prediction and reduction of lift-off acoustics for the H3 launch vehicle currently under development in Japan. The effect of vehicle elevation and shape of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b78b1afd70c63d18a84fa2a881997676
https://doi.org/10.1121/1.5137392
https://doi.org/10.1121/1.5137392
Autor:
Ayano Mori, Wataru Sarae, Keita Terashima, Seiji Tsutsumi, Hiroaki Kobayashi, Masao Takegoshi
Publikováno v:
The Journal of the Acoustical Society of America. 146:3040-3040
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e01681a9dc02d40a0ba8466122ad940
https://doi.org/10.1121/1.5137535
https://doi.org/10.1121/1.5137535
Autor:
Shinichi Maruyama, Wataru Sarae, Keita Terashima, Tatsuya Ishii, Tetsuo Hiraiwa, Seiji Tsutsumi
Publikováno v:
The Journal of the Acoustical Society of America. 144:1672-1672
Aero-vibro acoustic simulation for the prediction of harmful acoustic loading at lift-off of launch vehicle is developed. In this simulation technique, high-fidelity large-eddy simulation with computational aeroacoutics based on full-Euler equations
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::859ea8a2b5e234c0dca91cea9eefc1fb
https://doi.org/10.1121/1.5067450
https://doi.org/10.1121/1.5067450
Publikováno v:
The Journal of the Acoustical Society of America. 144:1673-1673
A subscale Acoustic test, the H3-scaled Acoustic Reduction Experiments (HARE), was conducted to predict liftoff acoustic environments of the H3 launch vehicle currently being developed in Japan. The HARE is based on 2.5% scale H3 vehicle models, whic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c8ff4ee173322489d6329fb1218a71b6
https://doi.org/10.1121/1.5067453
https://doi.org/10.1121/1.5067453
Investigation of Cryogenic Chilldown in a Complex Channel Under Low Gravity Using a Sounding Rocket.
Autor:
Kiyoshi Kinefuchi1, Wataru Sarae1, Yutaka Umemura2, Takeshi Fujita3, Koichi Okita4, Hiroaki Kobayashi5, Satoshi Nonaka6, Takehiro Himeno7, Tetsuya Sato8
Publikováno v:
Journal of Spacecraft & Rockets. Jan2019, Vol. 56 Issue 1, p91-103. 13p.