PDF Publication Title:
Text from PDF Page: 005
[8] Nagappan, N., Golubev, V. V., and Habashi, W., “Parametric Analysis of Icing Control Using Synthetic Jet Actuators,” AIAA Paper 2013-2453, 2013. https://doi.org/10.2514/6.2013-2453 [9] Shinkafi, A., and Lawson, C., “Enhanced Method of Conceptual Sizing of Aircraft Electro-Thermal De-Icing System,” International Journal of Mechanical, Aerospace, Industrial and Mechatronics Engineering, Vol. 8, No. 6, 2014, pp. 1069–1076. [10] Drury, M. D., Szefi, J. T., and Palacios, J. L., “Full-Scale Testing of a Centrifugally Powered Pneumatic De-Icing System for Helicopter Rotor Blades,” Journal of Aircraft, Vol. 54, No. 1, 2017, pp. 220–228. https://doi.org/10.2514/1.C033965 [11] De Pauw, D., and Dolatabadi, A., “Effect of Superhydrophobic Coating on the Anti-Icing and Deicing of an Airfoil,” Journal of Aircraft, Vol. 54, No. 2, 2017, pp. 490–499. https://doi.org/10.2514/1.C033828 [12] Liu, Y., Bond, L. J., and Hu, H., “Ultrasonic-Attenuation-Based Tech- nique for Ice Characterization Pertinent to Aircraft Icing Phenomena,” AIAA Journal, Vol. 55, No. 5, 2017, pp. 1602–1609. https://doi.org/10.2514/1.J055500 [13] Juuti, P., Haapanen, J., Stenroos, C., Niemelä-Anttonen, H., Harra, J., Koivuluoto, H., Teisala, H., Lahti, J., Tuominen, M., Kuusipalo, J., Vuoristo, P., and Mäkelä, J. M., “Achieving a Slippery, Liquid-Infused Porous Surface with Anti-Icing Properties by Direct Deposition of Flame Synthesized Aerosol Nano-Particles on a Thermally Fragile Substrate,” Applied Physics Letters, Vol. 110, No. 16, 2017, Paper 161603. https://doi.org/10.1063/1.4981905 [14] Moreau, E., “Airflow Control by Non-Thermal Plasma Actuators,” Jour- nal of Physics D: Applied Physics, Vol. 40, No. 3, 2007, pp. 605–636. https://doi.org/10.1088/0022-3727/40/3/S01 [15] Mertz, B. E., and Corke, T. C., “Single-Dielectric Barrier Discharge Plasma Actuator Modelling and Validation,” Journal of Fluid Mechan- ics, Vol. 669, Feb. 2011, pp. 557–583. https://doi.org/10.1017/S0022112010005203 [16] Wang, J. J., Choi, K. S., Feng, L. H., Jukes, T. N., and Whalley, R. D., “Recent Developments in DBD Plasma Flow Control,” Progress in Aerospace Sciences, Vol. 62, Oct. 2013, pp. 52–78. https://doi.org/10.1016/j.paerosci.2013.05.003 [17] Roupassov, D. V., Nikipelov, A. A., Nudnova, M. M., and Starikovskii, A. Y., “Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge,” AIAA Journal, Vol. 47, No. 1, 2009, pp. 168–185. https://doi.org/10.2514/1.38113 [18] Kelley, C. L., Bowles, P. O., Cooney, J., He, C., Corke, T. C., Osborn, B. A., Silkey, J. S., and Zehnle, J., “Leading-Edge Separation Control Using Alternating Current and Nanosecond Pulse Plasma Actuators,” AIAA Journal, Vol. 52, No. 9, 2014, pp. 1871–1884. https://doi.org/10.2514/1.J052708 [19] Zhang, X., Li, H. X., Huang, Y., and Wang, W. B., “Wing Flow Separation Control Using Asymmetrical and Symmetrical Plasma Actuator,” Journal of Aircraft, Vol. 54, No. 1, 2017, pp. 301–309. https://doi.org/10.2514/1.C033845 [20] Nishihara, M., Takashima, K., Rich, J. W., and Adamovich, I. V., “Mach 5 Bow Shock Control by a Nanosecond Pulse Surface Dielectric Barrier Discharge,” Physics of Fluid, Vol. 23, No. 6, 2011, pp. 605–622. https://doi.org/10.1063/1.3599697 [21] Hong, D., Magnier, P., Bauchire, J. M., Dong, B., and Pouvesle, J. M., “Experimental study of a DBD Surface Discharge for the Active Control of Subsonic Airflow,” Journal of Physics D: Applied Physics, Vol. 41, No. 15, 2008, Paper 155201. https://doi.org/10.1088/1361-6463/aa6229 [22] DeJoseph, C., Kimmel, R. L., Hayes, J. R., Menart, J., and Stanfield, S. A., “Rotational and Vibrational Temperature Distributions for a Dielectric Barrier Discharge in Air,” AIAA Journal, Vol. 47, No. 5, 2009, pp. 1107–1115. https://doi.org/10.2514/1.37648 [23] Joussot, R., Boucinha, V., Rabat, H., Hong, D., Leroy-Chesneau, A., and Weber-Rozenbaum, R., “Thermal Characterization of a DBD Plasma Actuator: Dielectric Temperature Measurements Using Infrared Thermography,” AIAA Paper 2010-5102, 2012. https://doi.org/10.2514/6.2010-5102 [24] Erfani, R., Zare-Behtash, H., and Kontis, K., “Plasma Actuator: Influ- ence of Dielectric Surface Temperature,” Experimental Thermal and Fluid Science, Vol. 42, Oct. 2012, pp. 258–264. https://doi.org/10.1016/j.expthermflusci.2012.04.023 [25] Meng, X., Chen, Z., and Song, K., “AC- and NS-DBD Plasma Flow Control Research,” Proceedings of the 2nd NPU-DLR Workshop on Aerodynamics, German Aerospace Center (DLR), German Aerospace Institute, Inst. fur Aerodynamik und Stromungstechnik, DLR-IB 124-2014/5, 1-75, Cologne, Germany, 2014. [26] Meng, X., Cai, J., Tian, Y., Han, X., Zhang, D., and Hu, H., “Experimental Study of Deicing and Anti-Icing on a Cylinder by DBD Plasma Actuation,” AIAA Paper 2016-4019, 2016. https://doi.org/10.2514/6.2016-4019 [27] Cai, J., Tian, Y., Meng, X., Han, X., Zhang, D., and Hu, H., “An Experimental Study of Icing Control Using DBD Plasma Actuator,” Experiments in Fluids, Vol. 58, No. 102, 2017, pp. 1–8. https://doi.org/10.1007/s00348-017-2378-y [28] Kriegseis, J., Simon, B., and Grundmann, S., “Towards In-Flight Applications? A Review on Dielectric Barrier Discharge-Based Boun- dary-Layer Control,” Applied Mechanics Reviews, Vol. 68, No. 2, 2016, Paper 020802. https://doi.org/10.1115/1.4033570 [29] Zhou, W., Liu, Y., Hu, H., Hu, H., and Meng, X., “Utilization of Thermal Effect Induced by Plasma Generation for Aircraft Icing Mitigation,” AIAA Journal, Vol. 56, No. 3, 2018, pp. 1097–1104. https://doi.org/10.2514/1.J056358 [30] Tian, Y., Zhang, Z., Cai, J., Yang, L., and Kang, L., “Experimental Study of an Anti-Icing Method over an Airfoil Based on Pulsed Dielectric Barrier Discharge Plasma,” Chinese Journal of Aeronautics, Vol. 31, No. 7, 2018, pp. 1449–1460. https://doi.org/10.1016/j.cja.2018.05.008 [31] Liu, Y., Kolbakir, C., Hu, H. Y., and Hu, H., “A Comparison Study on the Thermal Effects in DBD Plasma Actuation and Electrical Heating for Aircraft Icing Mitigation,” International Journal of Heat and Mass Transfer, Vol. 124, Sept. 2018, pp. 319–330. https://doi.org/10.1016/j.ijheatmasstransfer.2018.03.076 [32] Meng, X., Hu, H., Li, C., Abbasi, A. A., Cai, J., and Hu, H., “Mechanism Study of Coupled Aerodynamic and Thermal Effects Using Plasma Actuation for Anti-Icing,” Physics of Fluids, 31, No. 3, 2019, Paper 037103. https://doi.org/10.1063/1.5086884 [33] Roth, J. R., “Aerodynamic Flow Acceleration Using Paraelectric and Peristaltic Electrohydrodynamic Effects of a One Atmosphere Uniform Glow Discharge Plasma,” Physics of Plasmas, Vol. 10, No. 5, 2003, pp. 2117–2126. https://doi.org/10.1063/1.1564823 [34] Zhang, X., Li, H., Huang, Y., and Wang, W., “Wing Flow Separation Control Using Asymmetrical and Symmetrical Plasma Actuator,” Journal of Aircraft, Vol. 54, No. 1, 2017, pp. 301–309. https://doi.org/10.2514/1.C033845 [35] Corke, T. C., Post, M. L., and Orlov, D. M., “Single-Dielectric Barrier Discharge Plasma Enhanced Aerodynamics: Concepts Optimization, and Applications,” Journal of Propulsion and Power, Vol. 24, No. 5, 2008, pp. 935–945. https://doi.org/10.2514/1.24430 J. AIRCRAFT, VOL. 57, NO. 2: ENGINEERING NOTES 387 Downloaded by IOWA STATE UNIVERSITY on June 29, 2020 | http://arc.aiaa.org | DOI: 10.2514/1.C035697PDF Image | Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing Control
PDF Search Title:
Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing ControlOriginal File Name Searched:
2020-Haiyang-Plasma-J-Aircarft.pdfDIY PDF Search: Google It | Yahoo | Bing
NFT (Non Fungible Token): Buy our tech, design, development or system NFT and become part of our tech NFT network... More Info
IT XR Project Redstone NFT Available for Sale: NFT for high tech turbine design with one part 3D printed counter-rotating energy turbine. Be part of the future with this NFT. Can be bought and sold but only one design NFT exists. Royalties go to the developer (Infinity) to keep enhancing design and applications... More Info
Infinity Turbine IT XR Project Redstone Design: NFT for sale... NFT for high tech turbine design with one part 3D printed counter-rotating energy turbine. Includes all rights to this turbine design, including license for Fluid Handling Block I and II for the turbine assembly and housing. The NFT includes the blueprints (cad/cam), revenue streams, and all future development of the IT XR Project Redstone... More Info
Infinity Turbine ROT Radial Outflow Turbine 24 Design and Worldwide Rights: NFT for sale... NFT for the ROT 24 energy turbine. Be part of the future with this NFT. This design can be bought and sold but only one design NFT exists. You may manufacture the unit, or get the revenues from its sale from Infinity Turbine. Royalties go to the developer (Infinity) to keep enhancing design and applications... More Info
Infinity Supercritical CO2 10 Liter Extractor Design and Worldwide Rights: The Infinity Supercritical 10L CO2 extractor is for botanical oil extraction, which is rich in terpenes and can produce shelf ready full spectrum oil. With over 5 years of development, this industry leader mature extractor machine has been sold since 2015 and is part of many profitable businesses. The process can also be used for electrowinning, e-waste recycling, and lithium battery recycling, gold mining electronic wastes, precious metals. CO2 can also be used in a reverse fuel cell with nafion to make a gas-to-liquids fuel, such as methanol, ethanol and butanol or ethylene. Supercritical CO2 has also been used for treating nafion to make it more effective catalyst. This NFT is for the purchase of worldwide rights which includes the design. More Info
NFT (Non Fungible Token): Buy our tech, design, development or system NFT and become part of our tech NFT network... More Info
Infinity Turbine Products: Special for this month, any plans are $10,000 for complete Cad/Cam blueprints. License is for one build. Try before you buy a production license. May pay by Bitcoin or other Crypto. Products Page... More Info
| CONTACT TEL: 608-238-6001 Email: greg@infinityturbine.com | RSS | AMP |