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[16] Welch, G. E., Jones, S. M. and Paxson, D. E., 1997, “Wave Rotor-Enhanced Gas Turbine Engines,” Journal of Engineering for Gas Turbines and Power, 119, No. 2, pp. 469- 477. [17] Welch, G. E., 1997, “Macroscopic Balance Model for Wave Rotors,” Journal of Propulsion and Power, 13, No. 4, pp. 508-516. [18] Welch, G. E., 1997, “Two-Dimensional Computational Model for Wave Rotor Flow Dynamics,” Journal Engineering for Gas Turbines and Power, 119, No. 4, pp. 978-985. [19] Wilson, J., Paxson, D. E., 1996, “Wave Rotor Optimization for Gas Turbine Topping Cycles,” Journal of Propulsion and Power, 12, No. 4, pp. 778-785. See also SAE Paper 951411, 1995, and NASA TM 106951. [20] Welch, G. E., 2000, “Overview of Wave-Rotor Technology for Gas Turbine Engine Topping Cycles,” Novel Aero Propulsion Systems International Symposium, The Institution of Mechanical Engineers, pp. 2-17. [21] Wilson, J., 1997, “Design of NASA Lewis 4-Port Wave Rotor Experiment,” AIAA Paper 97-3139. Also NASA CR-202351. [22] Wilson J., Fronek, D., 1993, “Initial Results from the NASA-Lewis Wave Rotor Experiment,” AIAA Paper 93-2521. Also NASA TM-106148. [23] Wilson, J., 1997, “An Experiment on Losses in a Three Port Wave-Rotor,” NASA CR-198508. 24] Wilson, J., 1998, “An Experimental Determination of Loses in a Three-Port Wave Rotor,” Journal of Engineering for Gas Turbines and Power, 120, pp. 833-842. Also ASME Paper 96- GT-117, and NASA CR-198456. [25] Paxson, D. E., 1993, “A Comparison Between Numerically Modeled and Experimentally Measured Loss Mechanisms in Wave Rotors,” AIAA Paper 93-2522. [26] Paxson, D. E., 1995, “Comparison Between Numerically Modeled and Experimentally Measured Wave- Rotor Loss Mechanism” Journal of Propulsion and Power, 11, No. 5, pp. 908-914. Also NASA TM-106279. [27] Paxson D. E., Wilson, J., 1995, “Recent Improvements to and Validation of the One Dimensional NASA Wave Rotor Model,” NASA TM-106913. [28] Paxson, D. E., Nalim, M. R., 1999, “Modified Through-Flow Wave-Rotor Cycle with Combustor Bypass Ducts,” Journal of Propulsion and Power, 15, No. 3, pp. 462- 467. Also AIAA Paper 97-3140, and NASA TM-206971. [29] Nalim, M. R., Paxson, D. E., 1999, “Method and Apparatus for Cold-Gas Reinjection in Through-Flow and Reverse-Flow Wave Rotors,” US Patent 5894719. [30] Nalim, M. R., 1995, “Preliminary Assessment of Combustion Modes for Internal Combustion Wave Rotors,” AIAA Paper 95-2801. See also NASA TM 107000. [31] Nalim, R. M., and Paxson, D. E., 1997, “A Numerical Investigation of Premixed Combustion in Wave Rotors,” ASME Journal of Engineering for Gas Turbines and Power, 119, No. 3, pp. 668-675. See also ASME Paper 96-GT-116, 1996, and NASA TM 107242. [32] Nalim, M. R., Paxson, D. E., 1997, “Numerical Study of Stratified Charge Combustion in Wave Rotors,” AIAA Paper 97-3141. See also NASA TM 107513. [33] Nalim, M. R., 1999, “Assessment of Combustion Modes for Internal Combustion Wave Rotors,” ASME Journal of Engineering for Gas Turbines and Power, 121, No. pp. 265- 271. [34] Paxson, D. E., 2001, “A Performance Map for the Ideal Air Breathing Pulse Detonation Engine” AIAA Paper 2001-3465. See also NASA TM 2001-211085. [35] Wilson, J., Paxson, D. E., 2002, “On the Exit Boundary Condition for One-Dimensional Calculations of Pulse Detonation Engine Performance,” NASA TM 2002- 211299. [36] Shauer, F., Stutrud, J., and Bradley, R., 2001, “Detonation Initiation Studies and Performance Results for Pulse Detonation Engine Applications,” AIAA Paper 2001- 1129. [37] Shimo, M., Meyer, S. Heister, C., Weng, J. J. , and Gore, J., 2002, “An Experimental and Computational Study of Pulsed Detonations in a Single Tube,” AIAA Paper 2002-3716. [38] Seippel, C. ,1940 Swiss Patent 225426. [39] Seippel, C., 1942, Swiss Patent 229280. [40] Seippel, C., 1946, “Pressure Exchanger,” US Patent 2399394. [41] Seippel, C., 1949, “Gas Turbine Installation,” US Patent 2461186. [42] Azoury P. H., 1992, Engineering Applications of Unsteady Fluid Flow, John Wiley and Sons, New York. [43] Mayer, A., Oda, J., Kato, K., Haase, W. and Fried, R., 1989, “Extruded Ceramic - A New Technology for the Comprex® Rotor,” SAE Paper 890453. [44] Azoury, P. H., 1965-66, “An Introduction to the Dynamic Pressure Exchanger,” Proceedings of the Institution of Mechanical Engineers, 180, Part 1, No. 18, pp. 451-480. [45] Guzzella, L., Wenger, U., and Martin, R., 2000, “IC- Engine Downsizing and Pressure-Wave Supercharging for Fuel Economy,” SAE Paper 2000-01-1019. [46] Kentfield, J. A. C., 1998, “Wave Rotors and Highlights of Their Development” AIAA Paper 98-3248. [47] Akbari, P., Kharazi, A. A., and Müller, N., 2003, “Utilizing Wave Rotor Technology to Enhance the Turbo Compression in Power and Refrigeration Cycles,” 2003 International Mechanical Engineering Conference, ASME Paper IMECE2003-44222. [48] Kharazi, A. A., Akbari, P., and Müller, N., 2004, “An Application of Wave Rotor Technology for Performance Enhancement of R718 Refrigeration Cycles,” AIAA Paper 2004-5636. [49] Kharazi, A. A., Akbari, P., and Müller, N., 2004, “Performance Benefits of R718 Turbo-Compression Cycles Using a 3-Port Condensing Wave Rotors,” 2004 International Mechanical Engineering Conference, ASME Paper IMECE2004- 60992. [50] Kharazi, A. A., Akbari, P., and Müller, N., 2004, “Preliminary Study of a Novel R718 Turbo-Compression Cycle Using a 3-Port Condensing Wave Rotor,” 2004 International 10 Copyright © 2004 by ASMEPDF Image | RADIAL-FLOW WAVE ROTOR CONCEPTS, UNCONVENTIONAL DESIGNS
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