Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Said Boluriaan"'
Autor:
Philip J. Morris, Said Boluriaan
Publikováno v:
International Journal of Aeroacoustics. 2:255-292
This paper reviews the current state of knowledge of several classes of acoustic streaming. Acoustic streaming is classified based on the different mechanisms by which it is generated. For each category, the main achievements in terms of analysis, ex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06ab6a8a4bf670f6223bb569662eaf1c
https://doi.org/10.1260/147547203322986142
https://doi.org/10.1260/147547203322986142
Autor:
Said Boluriaan, Philip J. Morris
Publikováno v:
AIAA Journal. 40:2247-2256
Aparallelcodeisdevelopedtosimulatenumericallywakevortexdetectionusingaradioacousticsoundingsystem (RASS). The code is written in FORTRAN 90 with the message passing interface for parallel implementation. The numerical simulation solves simultaneously
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2cd2816bdfcf3fb75d5084c54e11cd7e
https://doi.org/10.2514/2.1587
https://doi.org/10.2514/2.1587
Publikováno v:
International Journal of Aeroacoustics. 1:17-41
Numerical simulations are presented for the unsteady flow and noise radiation of high speed circular jets. The predictions are based on solutions of the nonlinear disturbance equations. Only the large-scale fluctuations are resolved. The effects of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1bb01412c025461824898be6271c9dea
https://doi.org/10.1260/1475472021502659
https://doi.org/10.1260/1475472021502659
Autor:
Said Boluriaan, Philip J. Morris
Publikováno v:
AIAA Journal. 39:1097-1105
A parallel, two-dimensional Euler, one-dimensional Maxwell code is developed to numerically simulate wake vortex detection using a radio acoustic sounding system. The code is written in Fortran 90 with the message passing interface for parallel imple
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2fd05c332e31472f60c6055d1c1910c2
https://doi.org/10.2514/2.1422
https://doi.org/10.2514/2.1422
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
This paper describes a methodology for the simulation of high Reynolds number flow over rigid and moving bodies. The calculations are performed on a structured Cartesian grid regardless of the geometric complexity or motion of the body. The approach
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::335aba9f2aef6c07a3aca73dc0add6f8
https://doi.org/10.2514/6.2006-1089
https://doi.org/10.2514/6.2006-1089
Autor:
Philip J. Morris, Said Boluriaan
Publikováno v:
10th AIAA/CEAS Aeroacoustics Conference.
This paper describes a methodology for the prediction of jet noise based on data from a two-equation turbulence model. The noise model is an acoustic analogy based on the linearized Euler equations. Equivalent sources are included in both the continu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f57d253515adc0b507521406dc6fc486
https://doi.org/10.2514/6.2004-2977
https://doi.org/10.2514/6.2004-2977
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c6e0b63a8f91953b4a490ab14e6adca
https://doi.org/10.2514/6.2004-1126
https://doi.org/10.2514/6.2004-1126
Autor:
Said Boluriaan, Philip J. Morris
Publikováno v:
9th AIAA/CEAS Aeroacoustics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::479a8c48e13e3cfd2acaba8d4989a2f6
https://doi.org/10.2514/6.2003-3152
https://doi.org/10.2514/6.2003-3152
Autor:
Philip J. Morris, Said Boluriaan
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6b2282211a93500bacf4d5777015fe5
https://doi.org/10.2514/6.2003-367
https://doi.org/10.2514/6.2003-367
Autor:
Said Boluriaan, Philip J. Morris
Publikováno v:
8th AIAA/CEAS Aeroacoustics Conference & Exhibit.
A time accurate high order numerical simulation performed on parallel computers is used to study the minor losses due to an abrupt change in a resonator cross-sectional area. A finite amplitude standing wave is established in the resonator using two
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::005a343acc624b548728721627f8f749
https://doi.org/10.2514/6.2002-2594
https://doi.org/10.2514/6.2002-2594