This article presents the theory and operation of a null-type, inverted pendulum thrust stand. The thrust stand design supports thrusters having a total mass up to 250 kg and measures thrust over a range of 1 mN to 5 N. The design uses a conventional inverted pendulum to increase sensitivity, coupled with a null-type feature to eliminate thrust alignment error due to deflection of thrust. The thrust stand position serves as the input to the null-circuit feedback control system and the output is the current to an electromagnetic actuator. Mechanical oscillations are actively damped with an electromagnetic damper. A closed-loop inclination system levels the stand while an active cooling system minimizes thermal effects. The thrust stand incorporates an in situ calibration rig. The thrust of a 3.4 kW Hall thruster is measured for thrust levels up to 230 mN. The uncertainty of the thrust measurements in this experiment is +/-0.6%, determined by examination of the hysteresis, drift of the zero offset and calibration slope variation.

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This paper describes measurements of the dependence of lean blowout limits upon fuel composition for H2/CO/CH4 mixtures. Blowout limits were obtained at fixed approach flow velocity, reactant temperature, and combustor pressure at several conditions up to 4.4 atm and 470 K inlet reactants temperature. Consistent with prior studies, these results indicate that the percentage of H2 in the fuel dominates the mixture blowoff characteristics. That is, flames can be stabilized at lower equivalence ratios, adiabatic flame temperatures, and laminar flame speeds with increasing H2 percentage. Various methods of correlating these data were evaluated, using combinations of Lewis number (Lemix), adiabatic flame temperature (Tad), flame speed (SL), and chemical time (τchem). These correlations clearly indicate the significance of the mixture diffusivity, heat content, and flame propagation speed upon blowout characteristics across a wide fuel spectrum. Two basic models of flame stabilization discussed in the literature were evaluated — a well-stirred reactor based approach that considers the ratio of chemical and flow times, and a propagative mechanism that considers the ratio of flame and flow speed. Both mechanisms were able to correlate some, but not all segments of the data set.

A radio frequency argon microplasma jet at atmospheric-pressure is characterized using Langmuir probes. While optical methods are the typical diagnostic for these small scale plasmas, the simplicity and low cost of Langmuir probes makes them an attractive option. The plasma density and electron temperature are measured using existing high-pressure Langmuir probe theories developed for flames and arcs. The density and temperature vary from 1 × 1016 to 1 × 1019 m−3 and 2.3 to 4.4 eV, respectively, depending on the operating condition. The density decreases while the electron temperature increases with axial distance from the jet exit. The applicability of the probe theories as well as the effect of collisionality and jet mixing is discussed.

Reactive oxygen and nitrogen species (RONS) can influence plant signalling, physiology and development. We have previously observed that an argon plasma jet in atmospheric air can activate plant movements and morphing structures in the Venus flytrap and Mimosa pudica similar to stimulation of their mechanosensors in vivo. In this paper, we found that the Venus flytrap can be activated by plasma jets without direct contact of plasma with the lobe, midrib or cilia. The observed effects are attributed to RONS, which are generated by argon and helium plasma jets in atmospheric air. We also found that application of H 2 O 2 or HNO 3 aqueous solutions to the midrib induces propagation of action potentials and trap closing similar to plasma effects. Control experiments showed that UV light or neutral gas flow did not induce morphing or closing of the trap. The trap closing by plasma is thus likely to be associated with the production of hydrogen peroxide by the cold plasma jet in air. Understanding plasma control of plant morphing could help design adaptive structures and bioinspired intelligent materials.

Atmospheric pressure plasma jet (APPJ) based modification as a facile method to modify the intimal surface of small caliber nanofibrous tubular tissue scaffolds for potential use as vascular-graft or spinal-cord conduit is reported here. Polycaprolactone, a biomaterial used in the US Food and Drug Administration approved scaffolds for various tissue regeneration and bioabsorbable suture applications, was electrospun into thin nano/microfibers to form seamless three-dimensional (3D) conduits of 4 mm intimal diameter. The 3D conduits were subjected to treatment with an APPJ produced by dielectric barrier discharge using controlled gas flow into ambient atmosphere. He/air or He/air/NH3 gas mixtures combined with 8.5 kV pulsed direct current signal proved effective in creating a sustained and reactive cold plasma jet to modify the intimal surface of tubular scaffolds without affecting its biomechanical properties. The treatment resulted in surface chemistry modification as indicated by enrichment of oxygenated functional groups. Surface chemistry was determined via x-ray photoelectron spectroscopy. Scanning electron microscopy and glycerol contact angle measurements were used to determine the surface morphology and surface wettability. The data support the conclusion that APPJ is as an effective, facile, and robust approach to modify the intimal surface of small-caliber (<4 mm) tubular conduits (successfully accomplished and initially reported here) for potential applications in vascular and neural tissue engineering.