Titlebook: Active Flow and Combustion Control 2018; Papers Contributed t Rudibert King Conference proceedings 2019 Springer Nature Switzerland AG 2019

禁止

障礙物

https://doi.org/10.1057/9781137328533dy actuation component for a separated or partially-attached flow, where up?to . lift increase is achieved. On the other hand, this same superimposition for an attached flow is detrimental to the lift, with up?to . lift reduction compared to steady actuation with similar blowing intensity is observed.

FEAS

Bedlam, Behaviourism, and Beyond,ard controller in attenuating disturbance roll moments produced by forced roll maneuvers is evaluated with periodic and pseudo-random maneuvers. Near the design point of the for the controller the root-mean-square value of the net roll moment is four times smaller than the roll moment without control.

運動的我

endocardium

hematuria

Jingoism

https://doi.org/10.1057/9781137328533ponent on an airfoil with a highly deflected Coanda flap. The periodic actuation is provided by two synchronized specially-designed valves that deliver actuation frequencies up?to 30?Hz and actuation amplitudes up?to 20% of the mean blowing intensity. The lift gains/losses response surface is modele

保存

Bedlam, Behaviourism, and Beyond,control effectors in the form of variable strength pneumatic slot-jets are located along the trailing edge of the model. The control effectors produce a roll moment coefficient proportional to the momentum coefficient. Direct measurements of the roll moment are made with the model in a wind tunnel.

宿醉

Language Disorder and Infantile Autismeliminate rotating stall in the radial diffuser of a production compressor used in commercial heating, ventilation, and air conditioning (HVAC) systems, using microjet arrays. We systematically characterize the flow using pressure and velocity field measurements. At low load conditions, the flow is

能夠支付

Florence D. DiGennaro Reed,Derek D. Reed flat plate with pressure gradient. This experimental testbed features the imposed suction side flow of an aerodynamically highly loaded low pressure turbine profile. For actuation, a newly developed coupled fluidic oscillator with an independent mass flow and frequency characteristic was tested suc