Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Rogerio Pimentel"'
Publikováno v:
Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture.
Inlets are an essential element of aircraft propulsion systems. Aircraft with fuselage-embedded engines require intake ducts with bends to direct oncoming air into the engine. Consequently they often experience flow separation, losses, total pressure
Autor:
Grant Ingram, Asad Asghar, Courtney Rider, William D. E. Allan, Robert Stowe, Rogerio Pimentel
Publikováno v:
Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture.
This paper reports the investigation of a flow control strategy for an S-duct diffusers. The method incorporates stream-wise tubercles, and aims to enhance the performance of S-duct inlets by reducing the size and intensity of separated flow. These d
Autor:
S. C. Fabbro, Rogerio Pimentel, Yves de Villers, Tommy Ringuette, Nicole M. Houser, Philippe Lavoie
Publikováno v:
AIAA Journal. 56:2079-2085
A significant challenge associated with the implementation of plasma actuators for flow control is the high voltage signal required for their operation. In addition to logistical challenges, high voltage exposure from plasma actuators is a concern wi
Publikováno v:
IEEE Transactions on Plasma Science. 44:665-669
Dielectric-barrier-discharge plasma actuators have become very popular during the last decade. In aerodynamics, they have been employed for drag reduction, stability improvement, turbulence control, and so on. In this paper, the radar cross section (
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Autor:
Pierre Fournier, Richard Link, Robert Stowe, Tracy Smithson, Rogerio Pimentel, Derrick Alexander, Sophie Ringuette
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 14:29-56
Publikováno v:
Atomization and Sprays. 20:365-386
Publikováno v:
45th AIAA Plasmadynamics and Lasers Conference.
Publikováno v:
45th AIAA Plasmadynamics and Lasers Conference.
Phase-locked PIV has been used to investigate the time-dependent behaviour of a Dielectric Barrier Discharge (DBD) plasma actuator, excited by a sine-wave signal with peakto-peak amplitudes between 7.2 kV and 10 kV, and frequencies of 2.5 kHz and 4 k
Autor:
Nicolas Hamel, Rogerio Pimentel, Jan Vos, Francois Lesage, J.L.P.A. Moerel, Ronald Veraar, Daniel Corriveau, W.H.C. Halswijk
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, CO, USA, 2-5 August 2009 (Conference code: 81720)
Two research institutes TNO Defence, Security and Safety and DRDC-Valcartier have worked together on the improvement of modeling and simulation tools for the functioning of supersonic air intakes for realistic ramjet engines of tactical missiles. The
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