Repetitively Pulsed Nonequilibrium Plasmas for Magnetohydrodynamic Flow Control and Plasma-Assisted Combustion

• Published in: Journal of propulsion and power 2008-11, Vol.24 (6), p.1198-1215
• Main Authors: Adamovich, Igor V, Lempert, Walter R, Rich, J. William, Utkin, Yurii G, Nishihara, Munetake
• Format: Article
• Language: English
• ISSN: 0748-4658; 1533-3876
• DOI: 10.2514/1.24613

This paper demonstrates significant potential of the use of high-voltage, nanosecond pulse duration, high pulse repetition rate discharges for aerospace applications. The present results demonstrate key advantages of these discharges: 1) stability at high pressures, high flow Mach numbers, and high-energy loadings by the sustainer discharge, 2) high-energy fractions going to ionization and molecular dissociation, and 3) targeted energy addition capability provided by independent control of the reduced electric field of the direct current sustainer discharge. These unique capabilities make possible the generation of stable, volume-filling, low-temperature plasmas and their use for high-speed flow control, nonthermal flow ignition, and gasdynamic lasers. In particular, the crossed pulser-sustainer discharge was used for magnetohydrodynamic flow control in cold M=3M=3 flows, providing first evidence of cold supersonic flow deceleration by Lorentz force. The pulsed discharge (without sustainer) was used to produce plasma chemical fuel oxidation, ignition, and flameholding in premixed hydrocarbon-air flows, in a wide range of equivalence ratios and flow velocities and at low plasma temperatures, 150-300°C. Finally, the pulser-sustainer discharge was used to generate singlet oxygen in an electric discharge excited oxygen-iodine laser. Laser gain and output power are measured in the M=3M=3 supersonic cavity. [PUBLISHER ABSTRACT]