The smooth transition from field emission to a self-sustained plasma in microscale electrode gaps at atmospheric pressure
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Mihai A. Bilici↗
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Resolution of electron emission mechanisms in an argon arc with a hot tungsten cathode
The regenerative nature of the interaction between the electron emission processes at the cathode surface and the ion-, excited-atom-, and photon-production processes in the plasma was examined. Semiquantitative estimates of the thickness of the species production layer, the current partition, and the time constants were made. These results were used to interpret experimental measurements of the current decay of an argon arc at 46.7 kPa, 3.2-7.9 A, and 28-18 V, with a self-sustained hot tungsten cathode. After the discharge is suddenly connected to a voltage clamp, the disparity of decay rates for different emission processes permits the separation of thermionic emission from the faster-decaying components. The observed thermionic current constitutes about 30% of the total emission. The high nonthermionic portions of the current could not be explained in terms of the present understanding of the emission processes.
Chen, M. M.↗
Proposed distributed feedback crystal cavities for X-ray lasers
The use of zeolite crystals in distributed feedback crystal cavities for X-ray emissions is proposed. The zeolite crystals can guide the emitted X rays and can also generate the feedback necessary for self-sustained oscillation. A table lists the parameters of some typical zeolite crystals.
Elachi, C.↗
Some constraints on a greenhouse atmosphere for Triton
The possibility that a thick atmosphere exists around Neptune's satellite Triton is examined. The IR optical depth in the gray atmosphere approximation is computed for a range of possible surface compositions, albedos, and gravities. It is found that a self-sustaining optically-thick atmosphere is possible if molecular nitrogen and/or hydrogen are present. It is suggested that bimodal behavior of Triton's atmosphere is possible as seasonal effects and volatile distribution alter the distribution of thermal emission.
Nolan, Michael C.↗
Characterization and Simulation of the Thermoacoustic Instability Behavior of an Advanced, Low Emissions Combustor Prototype
Extensive research is being done toward the development of ultra-low-emissions combustors for aircraft gas turbine engines. However, these combustors have an increased susceptibility to thermoacoustic instabilities. This type of instability was recently observed in an advanced, low emissions combustor prototype installed in a NASA Glenn Research Center test stand. The instability produces pressure oscillations that grow with increasing fuel/air ratio, preventing full power operation. The instability behavior makes the combustor a potentially useful test bed for research into active control methods for combustion instability suppression. The instability behavior was characterized by operating the combustor at various pressures, temperatures, and fuel and air flows representative of operation within an aircraft gas turbine engine. Trends in instability behavior versus operating condition have been identified and documented, and possible explanations for the trends provided. A simulation developed at NASA Glenn captures the observed instability behavior. The physics-based simulation includes the relevant physical features of the combustor and test rig, employs a Sectored 1-D approach, includes simplified reaction equations, and provides time-accurate results. A computationally efficient method is used for area transitions, which decreases run times and allows the simulation to be used for parametric studies, including control method investigations. Simulation results show that the simulation exhibits a self-starting, self-sustained combustion instability and also replicates the experimentally observed instability trends versus operating condition. Future plans are to use the simulation to investigate active control strategies to suppress combustion instabilities and then to experimentally demonstrate active instability suppression with the low emissions combustor prototype, enabling full power, stable operation.
DeLaat, John C.↗
Characterization and Simulation of Thermoacoustic Instability in a Low Emissions Combustor Prototype
Extensive research is being done toward the development of ultra-low-emissions combustors for aircraft gas turbine engines. However, these combustors have an increased susceptibility to thermoacoustic instabilities. This type of instability was recently observed in an advanced, low emissions combustor prototype installed in a NASA Glenn Research Center test stand. The instability produces pressure oscillations that grow with increasing fuel/air ratio, preventing full power operation. The instability behavior makes the combustor a potentially useful test bed for research into active control methods for combustion instability suppression. The instability behavior was characterized by operating the combustor at various pressures, temperatures, and fuel and air flows representative of operation within an aircraft gas turbine engine. Trends in instability behavior vs. operating condition have been identified and documented. A simulation developed at NASA Glenn captures the observed instability behavior. The physics-based simulation includes the relevant physical features of the combustor and test rig, employs a Sectored 1-D approach, includes simplified reaction equations, and provides time-accurate results. A computationally efficient method is used for area transitions, which decreases run times and allows the simulation to be used for parametric studies, including control method investigations. Simulation results show that the simulation exhibits a self-starting, self-sustained combustion instability and also replicates the experimentally observed instability trends vs. operating condition. Future plans are to use the simulation to investigate active control strategies to suppress combustion instabilities and then to experimentally demonstrate active instability suppression with the low emissions combustor prototype, enabling full power, stable operation.
DeLaat, John C.↗
Measurements of kinetic processes in a self-sustained discharge XeF laser
Measurements are presented for processes occurring in XeF self-sustained discharges including fluorescence, gain, and absorption at different wavelengths as a function of F2, Xe, and He partial pressures. Time-correlated oscillograms are given for the laser discharge current, metastable XeF small-signal gain at 351.1 nm, transient absorptions at 333.6 and 363.8 nm, metastable-XeF B-state sidelight emission at about 350 nm, metastable-F emission at 634.8 nm, and metastable-F emission at 731.1 nm. It is found that He atoms are necessary for the production of metastable-XeF in its lower vibrational levels and that radiative processes and He quenching are the primary mechanisms for metastable-XeF decay. For small-signal gains of as low as about 8%/cm, the transient absorption at the laser wavelength may be as large as about 1-2%/cm.
Gower, M. C.↗