In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …

This paper provides an overview of modern research on magnetoplasma methods of
influencing gas-dynamic and plasma flows. The main physical mechanisms that control the …

Active flow control is a topic in full expansion due to associated industrial applications of
huge importance, particularly for aeronautics. Among all flow control methods, such as the …

Nomenclature b= model chord length, m Cd= drag coefficient Cl= lift coefficient Cp=
pressure coefficient c= airfoil thickness, mf= repetition frequency, Hz I= electric current, A l …

This paper presents a detailed explanation of the physical mechanism of the nanosecond
pulsed surface dielectric barrier discharge (SDBD) effect on the flow. Actuator-induced gas …

Localized arc filament plasma actuators are used to control an axisymmetric Mach 1.3
ideally expanded jet of 2.54 cm exit diameter and a Reynolds number based on the nozzle …

A= Electrode area, square meters. K= Dielectric heating constant, Watts/kilovolt2-Hertz. P=
Dielectric power loss, Watts. Urms, Umax= RMS and maximum voltage between the …

A parallel 2D code for modeling nanosecond surface dielectric barrier discharge (nSDBD),
combining a discharge description, detailed kinetics and hydrodynamics, is developed and …

A Dielectric Barrier Discharge (DBD) is mounted at the leading edge of a NACA 0015 airfoil
model. The effects of steady and unsteady actuations on the lift and drag coefficients are …

A detailed physical model for asymmetric dielectric barrier discharge (DBD) in air at low
voltages (1.5–2 kV) is developed. Modeling of DBD with an applied sinusoidal voltage is …