Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Takeo Okunuki"'
Autor:
Susumu Teramoto, Takeo Okunuki, Masahito Akamine, Kent L. Gee, Koji Okamoto, Tracianne B. Neilsen, Seiji Tsutsumi
Publikováno v:
AIAA Journal. 56:1943-1952
For an adequate understanding of the broadband acoustic phenomena generated by a rocket exhaust jet impinging on a flame deflector, this study experimentally clarifies the factors that cause the di...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ef49bf1f86fec1fbd246f0f6d33b4ad
https://doi.org/10.2514/1.j056504
https://doi.org/10.2514/1.j056504
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 59:287-294
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a883c5eec88b1054998a3e72b86143db
https://doi.org/10.2322/tjsass.59.287
https://doi.org/10.2322/tjsass.59.287
Autor:
Seiji Tsutsumi, Takeo Okunuki, Koji Okamoto, Masahito Akamine, Yuta Nakanishi, Susumu Teramoto
Publikováno v:
AIAA Journal. 53(7):2061-2067
Accepted: 2014-11-04
資料番号: SA1150163000
資料番号: SA1150163000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6b452020e7725432e09479eeee145c6d
http://id.nii.ac.jp/1696/00028836/
http://id.nii.ac.jp/1696/00028836/
Autor:
Seiji Tsutsumi, Susumu Teramoto, Takeo Okunuki, Koji Okamoto, Mylan R. Cook, Tracianne B. Neilsen, Kent L. Gee, Masahito Akamine
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7e36a81e204df28b0ace662899d9393f
https://doi.org/10.2514/6.2017-3519
https://doi.org/10.2514/6.2017-3519
Autor:
Seiji Tsutsumi, Takeo Okunuki, Koji Okamoto, Tracianne B. Neilsen, Kent L. Gee, Susumu Teramoto, Masahito Akamine
Publikováno v:
22nd AIAA/CEAS Aeroacoustics Conference.
For an adequate understanding of the broadband acoustic phenomena generated by a rocket exhaust jet impinging on a flame deflector, this study experimentally clarifies the factors that cause the di...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8668c031c25136d53b0a0080a67403d
https://doi.org/10.2514/6.2016-2930
https://doi.org/10.2514/6.2016-2930
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 51:139-145
Flows over two circular cylinders in tandem, side-by-side, and staggered arrangements were analyzed using the overset grid method, which is capable of handling a variety of sizes and arrangements. The Reynolds number was 100 based on the cylinder dia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fb46c8ab4e3e62bf97b9f9e1731444c9
https://doi.org/10.2322/tjsass.51.139
https://doi.org/10.2322/tjsass.51.139
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 46:113-120
Three types of devices were tested for their effects in reducing the strong adverse pressure gradient in a closed-type cavity with a depth of 8 mm and length-to-depth ratio of 15. The first type of control device consisted of embedding arrays of tube
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a76aa74bc85f232afaa7927f26c70f8d
https://doi.org/10.2322/tjsass.46.113
https://doi.org/10.2322/tjsass.46.113
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 45:170-179
Compressible flows over cavities with a series value of length-to-depth ratio (L⁄D) were investigated experimentally, with the objective being to elucidate the mechanism of the transition of types of cavity flows as their L⁄D increases or decreas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f4142bf6b4dc34792045a958a298bf06
https://doi.org/10.2322/tjsass.45.170
https://doi.org/10.2322/tjsass.45.170
Autor:
Seiji Tsutsumi, Takeo Okunuki, Koji Okamoto, Masahito Akamine, Yuta Nakanishi, Susumu Teramoto
Publikováno v:
52nd Aerospace Sciences Meeting.
Acoustic and flow fields of a Mj = 1.8 correctly-expanded jet impinging on a 45○ inclined flat plate are investigated experimentally. In the experiments, microphone measurement, Schlieren visualization, and wall static pressure measurement on the i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cd56feec7063b6bb21f007699e85e67
https://doi.org/10.2514/6.2014-0879
https://doi.org/10.2514/6.2014-0879
Autor:
Koji Okamoto, Tracianne B. Neilsen, Seiji Tsutsumi, Masahito Akamine, Kent L. Gee, Takeo Okunuki, Susumu Teramoto
Publikováno v:
The Journal of the Acoustical Society of America. 140:3043-3043
The authors have studied the acoustic wave from an unheated, Mach 1.8 ideally expanded jet by using the acoustic intensity vector measurement and analysis of high-speed schlieren visualization movies (for example, the Fourier transform and wavelet-ba
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94ab0a57d7a850e86f5ac5c2b3877b76
https://doi.org/10.1121/1.4969450
https://doi.org/10.1121/1.4969450