Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Seyed Gholamali Saddoughi"'
Autor:
I. V. Chernysheva, Boris Potapkin, Igor' V Kochetov, Seyed Gholamali Saddoughi, John Thomas Herbon, Anatoly P. Napartovich, M. I. Strelkova, A. E. Baranov, S. Ya. Umanskii, M. A. Deminskii, Timothy John Sommerer
Publikováno v:
Russian Journal of Physical Chemistry B. 7:410-423
A plasma-chemical kinetic mechanism of the low-temperature (600 < T < 1000 K) oxidation/combustion of methane under conditions of nonequilibrium plasma over a wide pressure range (P = 0.1−100 atm) is developed and verified. The mechanism is compris
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::807317a42cb4b4a89675da2ab48215d0
https://doi.org/10.1134/s1990793113040040
https://doi.org/10.1134/s1990793113040040
Autor:
Stanton Earl Weaver, Todd Garrett Wetzel, Seyed Gholamali Saddoughi, Jivtesh Garg, Mehmet Arik
Publikováno v:
Journal of Electronic Packaging. 127:503-511
Microfluid devices are conventionally used for boundary layer control in many aerospace applications. Synthetic jets are intense small-scale turbulent jets formed from periodic entrainment and expulsion of the fluid in which they are embedded. The je
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72b1f35804a1685ef3100f5149bd38b0
https://doi.org/10.1115/1.2065727
https://doi.org/10.1115/1.2065727
Autor:
Seyed Gholamali Saddoughi, Aspi Rustom Wadia, Grover Andrew Bennett, Steven L. Puterbaugh, Matthew Patrick Boespflug
Publikováno v:
Volume 2A: Turbomachinery.
Blade tip losses represent a major performance penalty in low aspect ratio transonic compressors. This paper reports on the experimental evaluation of the impact of tip clearance with and without plasma actuator flow control on performance of an U.S.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::620d1ebeeb7c0dff706d93447fa5671d
https://doi.org/10.1115/gt2014-25294
https://doi.org/10.1115/gt2014-25294
Autor:
Aspi Rustom Wadia, Robert Carl Murray, Giridhar Jothiprasad, Katherine Essenhigh, Grover Andrew Bennett, Andrew Breeze-Stringfellow, Seyed Gholamali Saddoughi
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
This research investigates different dielectric barrier discharge (DBD) actuator configurations for affecting tip leakage flow and suppressing stall inception. Computational investigations were performed on a low-speed rotor with a highly loaded tip
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ba3495299acd7fbadfe0ae7050cfe8d1
https://doi.org/10.1115/gt2010-22345
https://doi.org/10.1115/gt2010-22345
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
Aircraft Carrier landing approach makes unique demands upon a Naval Aircraft by restricting the maximum permissible angle of attack and approach speed during landing. For a fixed geometry, these factors define the maximum landing weight of the vehicl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5885ce2ef8d21cbf18d0e7e2c95aa451
https://doi.org/10.2514/6.2009-885
https://doi.org/10.2514/6.2009-885
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.
** Wakes of aircraft external stores can generate high acoustic loads on downstream structures that lead to fatigue and failure of structural components. Structural vibration control systems have been employed to dampen structural loads but can becom
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0916393e79e3783e320bbedae0c51e4e
https://doi.org/10.2514/6.2007-878
https://doi.org/10.2514/6.2007-878
Publikováno v:
3rd AIAA Flow Control Conference.
Pods and externally carried stores can generate unsteady flows in their wakes with high acoustic loads capable of damaging aircraft structure. Active flow control technology has the potential to modify unsteady shedding in the wake of the pod, thereb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::834de614dc50c6794041f98894d64848
https://doi.org/10.2514/6.2006-3185
https://doi.org/10.2514/6.2006-3185
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73cfb59640aa1a0a0df707b8c4bbb397
https://doi.org/10.2514/6.2006-439
https://doi.org/10.2514/6.2006-439
Autor:
D Opaits, Dmitry Roupassov, Ivan Zavialov, Seyed Gholamali Saddoughi, Andrei Starikovskii, Svetlana Starikovskaia
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86db9b2099f18b669010c8a3467e47b4
https://doi.org/10.2514/6.2005-1180
https://doi.org/10.2514/6.2005-1180
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Pods and externally carried stores can generate unsteady flows in their wakes with high acoustic loads capable of damaging aircraft structure. Active flow control technology has the potential to modify unsteady shedding in the wake of the pod, thereb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::50259df3336a17460c73879c9ef679bc
https://doi.org/10.2514/6.2005-799
https://doi.org/10.2514/6.2005-799