In the present survey, various methods for the acoustic design of aeroengine nacelle are first briefly introduced along with the comments on their advantages an
Numerical approach of hybrid laminar flow control(HLFC) is investigated for the suction hole with a width between 0.5 mm and 7 mm. The accuracy of Menter and La
A 15° swept wing with dielectric barrier discharge plasma actuator is designed.Experimental study of flow separation control with nanosecond pulsed plasma actu
Experimental investigation of aerodynamic control on a 35 swept flying wing by means of nanosecond dielectric barrier discharge(NS-DBD) plasma was carried out a
Mesenteric lymphadenopathy is a rare manifestation of Gaucher disease (GD) with only 26 cases reported worldwide and its outcome remains largely unknown.In this