Fundamentals of jet propulsion with applications

Fundamentals of Jet Propulsion with Applications

Volumn , Issue , 2005, Pages 1-637

  Flack, Ronald D ^a  

^a UNIVERSITY OF VIRGINIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EDUCATION; FLUID MECHANICS; PROPULSION; STUDENTS; THERMODYNAMICS;

COMPONENT DESIGN; CYCLE ANALYSIS; GRADUATE STUDENTS; JET PROPULSION; OPERATING PRINCIPLES; PRACTICING ENGINEERS; SYSTEM MATCHING; TEACHING TOOLS;

AIRCRAFT PROPULSION;

EID: 85010465396     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1017/CBO9780511807138     Document Type: Book

References (125)

1. Abbott, I. H., and von Doenhoff, A. E. (1959). Theory of Wing Sections, Dover Publications, New York, NY.
2. Adamczyk, J. J. (2000). Aerodynamic analysis of multistage turbomachinery flows in support of aerodynamic design. ASME Transactions, Journal of Turbomachinery. 122 (2), 189-217.
3. Adler, D. (1980). Status of centrifugal impeller internal dynamics, parts I and II. Transactions ASME, Journal of Engineering for Power. 102 (3), 728-746.
4. Ainley, D. G., and Mathieson, G. C. R. (1951). A method of performance estimation for axial flow turbines. Aeronautical Research Council, R&M No. 2974.
5. Anderson, J. D. (1982). Modern Compressible Flow with Historical Perspective. McGraw-Hill, New York.
6. Ashley, S. (1997). Turbines on a Dime. Mechanical Engineering. 119 (10), 78-81.
7. ASME International History and Heritage (1997). Landmarks in Mechanical Engineering. Purdue University Press, West Lafayette, IN.
8. Aungier, R. H. (2000). Centrifugal Compressors-A Strategy for Aerodynamic Design and Analysis. ASME Press, New York, NY.
9. Bacha, J., Barnes, F., Franklin, M., Gibbs, L., Hemighaus, G., Hogue, N., Lesnini, D., Lind, J., Maybury, J., and Morris, J. (2000). Aviation Fuels Technical Review. Chevron Products Company, FTR-3.
10. Balje, O. E. (1981). Turbomachines. Wiley, New York, NY.
11. Billington, D. P. (1996). The Innovators. Wiley, New York, NY.
12. Boyce, M. P. (1982). Gas Turbine Engineering Handbook. Gulf Publishing Co., Houston, TX.
13. Brennen, C. E. (1994). Hydrodynamics of Pumps. Concepts ETI & Oxford, Norwich, VT.
14. Busemann, A. (1928). Das Förderhöhenverhältnis radialer Kreiselpumpen mit logrithmischspiraligen Schaufeln. Zeitschrift für Angewandte Mathematik und Mechanik. 8, 372-384.
15. Caruthers, J. E., and Kurosaka, M. (1982). Flow Induced Vibration of Diffuser Excited Radial Compressors. NASA NAG No. 3-86.
16. Chase, M. W. (1998), NIST-JANAF Thermochemical Tables, 4th Edition, Journal of Physical and Chemical Reference Data Monographs & Supplements, Monograph No. 9, AIP Press, New York, NY.
17. Cohen, H., Rogers, G. F. C., and Saravanamuttoo, H. I. H. (1996). Gas Turbine Theory, 4th ed. Longman Group, Essex, UK.
18. Cumpsty, N. (1997). Jet Propulsion. Cambridge, Cambridge, UK.
19. Cumpsty, N. A. (1977). Critical review of turbomachinery noise. Transactions of ASME, Journal of Fluids Engineering. 99(2), 278-293.
20. Cumpsty, N. A. (1988). Compressor Aerodynamics. Longman Group, Essex, UK.
21. Department of the U. S. Navy (1953). Handbook of Supersonic Aerodynamics, Vol. 5. Bureau of Ordnance, Washington, DC.
22. Dixon, S. L. (1975). Worked Examples in Turbomachinery. Pergamon Press, Oxford, UK.
23. Dixon, S. L. (1998). Fluid Mechanics and Thermodynamics of Turbomachinery, 4th ed. Butterworths, Boston, MA.
24. Dring, R. P., Joslyn, H. D., Hardin, L. W., and Wagner, J. H. (1982). Turbine rotor-stator interaction. 27th ASME International Gas Turbine Exposition. ASME Paper No. 82-GT-3.
25. Dunham, J. (2000). A. R. Howell-Father of the British axial compressor. ASME TURBOEXPO 2000, May 8-11, Munich, Germany. ASME Paper No. 2000-GT-8.
26. Dunn, M. G. (2001). Convective heat transfer and aerodynamics in axial flow turbines. ASME TURBO EXPO 2001, New Orleans, LA. ASME Paper No. 2001-GT-0506.
27. Eckardt, D. (1975). Instantaneous measurements in the jet-wake discharge flow of a centrifugal compressor impeller. ASME Transactions, Journal of Engineering for Power. 91 (3), 337-345.
28. El-Masri, M. A. (1988). GASCAN-An interactive code for thermal analysis of gas turbine systems. ASME Transactions, Journal of Engineering for Gas Turbines and Power. 110 (2), 201-209.
29. Elmendorf, W., Mildner, F., Röper, R., Krüger, U., and Kluck, M. (1998). Three-dimensional analysis of a multistage compressor flow field. TURBO EXPO 1998, Stockholm, Sweden. ASME Paper 98-GT-249.
30. Engeda, A. (1998). Early historical development of the centrifugal impeller. TURBO EXPO 1998, Stockholm, Sweden. ASME Paper 98-GT-22.
31. Fielding, L. (2000). Turbine Design-The Effect of Axial Flow Turbine Performance of Parameter Variation. ASME Press, New York, NY.
32. Flack, R. D., and Thompson, H. D. (1975). Comparison of pressure and LDV velocity measurements with predictions in transonic flow. AIAA Journal. 13 (1), 53-59.
33. Flack, R. D. (1987). Classroom analysis and design of axial flow compressors using a streamline analysis method. International Journal of Turbo and Jet Engines. 4 (3-4), 285-296.
34. Flack, R. D. (1990) Analysis and matching of gas turbine components. International Journal of Turbo and Jet Engines. 7, 217-226.
35. Flack, R. (2002). Component matching analysis for a power generation gas turbine-Classroom applications. ASME TURBO EXPO 2002, June 3-6, 2002, Amsterdam, The Netherlands. ASME Paper No. GT-2002-30155.
36. Flack, R. D., (2004), "Component Matching Analysis for a Twin Spool Turbofan," 10th International Symposium onTransport Phenomena and Dynamics of Rotating Machinery (ISROMAC-10), March 7-11, Honolulu, Hawaii, Paper No. ISROMAC10-2004-067.
37. Fox, R. W., and Kline, S. J. (1962). Flowregime data and design methods for curved subsonic diffusers. Transactions ASME, Journal of Basic Engineering. 84, 303-312.
38. Glassman, A. J. (1972a, 1973, and 1975). Turbine Design and Application, Vols. 1, 2, and 3. NASA SP-290.
39. Glassman, A. J. (1972b). Computer Program for Preliminary Design Analysis of Axial Flow Turbines. NASA SP-6702.
40. Hah, C. (1997). Turbomachinery Fluid Dynamics and Heat Transfer. Marcel-Dekker, New York, NY.
41. Haines, A. B., MacDougall, A. R. C., and Monaghan, R. J. (1946). Charts for the Determination of the Performance of a Propeller under Static, Take-off, Climbing, and Cruising Conditions. Aeronautical Research Council. R&M No. 2086.
42. Han, J. C., Dutta, S., and Ekkad, S. (2000). Gas Turbine Heat Transfer and Cooling. Taylor and Francis, New York, NY.
43. Hawthorne, W. R. (1964). Aerodynamics of Turbines and Compressors. Princeton, Princeton, NJ.
44. Heppenheimer, T. A. (1993). The Jet Engine. Invention and Technology. 9 (2), 44-57.
45. Hesse, W. J., and Mumford, N. V. J. (1964). Jet Propulsion for Aerospace Applications. Pitman Publishing, New York, NY.
46. Hill, P. G., and Peterson, C. R. (1992). Mechanics and Thermodynamics of Propulsion, 2d ed. Addison Wesley, Reading, MA.
47. Horlock, J. H. (1958). Axial Flow Compressors. Krieger, Malabar, FL.
48. Horlock, J. H. (1966). Axial Flow Turbines. Krieger, Malabar, FL.
49. Howarth, L. (ed.) (1953). Modern Developments in Fluid Dynamics, High Speed Flow. Oxford, Oxford, UK.
50. Howell, A. R. (1942). The present basis of axial compressor design: Part I-Cascade theory and performance. Aeronautical Research Council. R&M No. 2095.
51. Howell, A. R. (1945a). Fluid dynamics of axial compressors. Proceedings of the Institution of Mechanical Engineers. 153 (12), 441-452.
52. Howell, A. R. (1945b). Design of axial compressors. Proceedings of the Institution of Mechanical Engineers. 153 (12), 452-462.
53. Japikse, D., and Baines, N. C. (1994). Introduction to Turbomachinery. Concepts ETI & Oxford, Norwich, VT.
54. Johnsen, I. A., and Bullock, R. O. (1965). Aerodynamics Design of Axial-Flow Compressors, Revised. NASA SP-36.
55. Karassik, I. J., Krutzsch, W. C., Fraser, W. H., Messina, J. P. (1976). Pump Handbook. McGraw-Hill, New York, NY.
56. Keenan, J. H. (1970). Thermodynamics. Wiley, New York, NY.
57. Keenan, J. H., Chao, J., and Kaye, J. (1983). Gas Tables, 2d ed. Wiley, New York, NY.
58. Kercher, D. M. (1998). Afilm coolingCFDbilbiography: 1971-1996. International Journal of Rotating Machinery. 4 (1), 61-72.
59. Kercher, D. M. (2000). Turbine airfoil leading edge film cooling bibliography: 1972-1998. International Journal of Rotating Machinery. 6 (5), 313-319.
60. Kerrebrock, J. L. (1992). Aircraft Engines and Gas Turbines, 2d ed. MIT Press, Cambridge, MA.
61. Kurzke, J. (1995). Advanced user-friendly gas turbine performance calculations on a personal computer. ASME TURBOEXPO 1995, June 5-8, Houston, TX. ASME Paper No. 95-GT-147.
62. Kurzke, J. (1996). How to get component maps for aircraft gas turbine performance calculations. ASME TURBOEXPO 1996, June 10-13, Birmingham, UK. ASME Paper No. 96-GT-164.
63. Kurzke, J. (1998). Gas turbine cycle design methodology: A comparison of parameter variation with numerical optimization. ASME TURBOEXPO 1998, June 2-5, Stockholm, Sweden. ASME Paper No. 98-GT-343.
64. Lefebvre, A. H. (1983). Gas Turbine Combustion. Hemisphere Publishing, New York, NY.
65. LeJambre, C. R., Zacharias, R. M., Biederman, B. P., Gleixner, A. J., and Yetka, C. J. (1998). Development and application of a multistage Navier-Stokes solver: Part II-Application to a high-pressure compressor design. ASME Transactions, Journal of Turbomachinery. 120 (2), 215-223.
66. Liepmann, H. W., and Roshko, A. (1957). Elements of Gas Dynamics. Wiley, New York, NY.
67. Lloyd, P. (1945). Combustion in the gas turbine. Proceedings of the Institution of Mechanical Engineers. 153 (12), 462-472.
68. Logan, E. (1993). Turbomachinery-Basic Theory and Applications, 2d ed. Marcel Dekker, New York, NY.
69. Maccoll, J. W. (1937). The conical shock wave formed by a cone moving at high speed. Proceedings of the Royal Society of London, Series A. 159, 459-472.
70. Malecki, R. E., Rhie, C. M., McKinney, R. G., Ouyang, H., Syed, S. A., Colket, M. B., and Madabhushi, R. K. (2001). Application of an advanced cfd-based analysis system to the pw6000 combustor to optimize exit temperature distribution-Part I: Description and validation of the analysis tool. TURBO EXPO 2001, New Orleans, LA. ASME Paper No. 2001-GT-0062.
71. Mattingly, J. D. (1996). Elements of Gas Turbine Propulsion. McGraw-Hill, New York, NY.
72. Mattingly, J. D., Heiser, W. H., and Daley, D. H. (1987). Aircraft Engine Design. AIAA Education Series, Reston, VA.
73. Meher-Homji, C. B. (1996). The development of the Junkers Jumo 004B-The world's first production turbojet. ASME TURBO EXPO 1996, June 10-13, Birmingham, UK. ASME Paper No. 96-GT-457.
74. Meher-Homji, C. B. (1997a). The development of the Whittle turbojet. ASME TURBO EXPO 1997, Orlando, Florida. ASME Paper No. 97-GT-528.
75. Meher-Homji, C. B. (1997b). Anselm Franz and the Jumo 004. Mechanical Engineering. 119 (9), 88-91.
76. Meher-Homji, C. B. (1999). Pioneering turbojet developments of Dr. Hans von Ohain-From the HeS 1 to the HeS 011. ASME TURBO EXPO 1999, June 7-10, Indianapolis, IN. ASME Paper No. 99-GT-228.
77. Merzkirch, W. (1974). Flow Visualization. Academic Press, New York, NY.
78. Miner, S. M., Beaudoin, R. J., and Flack, R. D. (1989). Laser velocimeter measurements in a centrifugal flow pump. ASME Transactions, Journal of Turbomachinery. 111 (3), 205-212.
79. Mirza-Baig, F. S., and Saravanamuttoo, H. I. H. (1991). Off-design performance prediction of turbofans using gasdynamics. 36th ASME International Gas Turbine Exposition, 1991, June 3-6, Orlando, FL. ASME Paper No. 91-GT-389.
80. Moody, L. F. (1944). Friction factors for pipe flow. Transactions of the ASME. 66 (8), 671-684.
81. Oates, G. C. (1997). Aerothermodynamics of Gas Turbine and Rocket Propulsion, 3d ed. AIAA Education Series, Reston, VA.
82. Oates, G. C. (ed.) (1985). Aerothermodynamics of Aircraft Engine Components. AIAA Education Series, Reston, VA.
83. Oates, G. C. (ed.) (1989). Aircraft Propulsion Systems Technology and Design. AIAA Education Series, Reston, VA.
84. Olson, W. T., Childs, J. H., and Jonash, E. R. (1955). The combustion-efficiency problem of the turbojet at high altitude. Transactions of the ASME. 77, 605-615.
85. Osborn, W. C. (1977). Fans, 2d ed. Pergamon Press, Oxford, UK.
86. Peters, J. E. (1988). Current gas turbine combustion and fuels research and development. AIAA Journal of Propulsion. 4 (3), 193-206.
87. Pfleiderer, C. (1961). Pumps. Springer-Verlag, Berlin.
88. Pratt&Whitney (1988). The Aircraft Gas Turbine Engine and Its Operation, Revised ed. P&WOperations Manual 200, E. Hartford, CT.
89. Reed, J. A., and Afjeh, A. A. (2000). Computational simulation of gas turbines: Part 1-Foundations of componentbased models and part 2-Extensible domain framework. ASME Transactions, Journal of Engineering for Gas Turbines and Power. 122 (3), 366-386.
90. Reynolds, W. C. (1986). STANJAN: The Element Potential Method for Chemical Equilibrium Analysis. Thermosciences Division, Department of Mechanical Engineering, Stanford University, Palo Alto, CA.
91. Rhie, C. M., Gleixner, A. J., Spear, D. A., Fischberg, C. J., and Zacharias, R. M. (1998). Development and application of a multistage Navier-Stokes solver: Part I-Multistage modeling using bodyforces and deterministic stresses. ASME Transactions, Journal of Turbomachinery. 120 (2), 205-214.
92. Rolls-Royce (1996). The Jet Engine, 5th ed. Rolls-Royce Technical Publication Department, Derby, UK.
93. St. Peter, J. (1999). History of Aircraft Gas Turbine Engine Development in The United States: A Tradition of Excellence. ASME International, New York, NY.
94. Saito, Y., Sugiyama, N., Endoh, M., and Matsuda, Y. (1993). Conceptual study of separated core ultrahigh bypass engine. Journal of Propulsion and Power. 9 (6), 867-873.
95. Shapiro, A. H. (1953). The Dynamics and Thermodynamics of Compressible Fluid Flow, Volumes 1 and 2. Ronald, New York, NY.
96. Shepherd, D. G. (1956). Principles of Turbomachinery. Macmillan, New York, NY.
97. Shih, T. I. P., and Sultanian, B. K. (2001). Computations of internal and film cooling," Chapter 5, 175-225, in Heat Transfer in Gas Turbines, Sunden, B. and Faghari, M. (eds.). WIT Press, Southampton, UK.
98. Stanitz, J. D. (1952). Some theoretical aerodynamic investigations of impellers in radial and mixed-flowcentrifugal impellers. ASME Transactions. 74, 473-497.
99. Stepanoff, A. J. (1957). Centrifugal and Axial Flow Pumps. Wiley, New York, NY.
100. Stodola, A. (1927). Steam and Gas Turbines, Vols. 1 and 2. McGraw-Hill, New York, NY (also Peter Smith Publisher, Gloucester, MA., 1945).
101. Theodorsen, T. (1948). Theory of Propellers. McGraw-Hill, New York, NY.
102. Traupel, W. (1958). Thermische Turbomaschinen. Springer-Verlag, Berlin.
103. Treager, I. E. (1979). Aircraft Gas Turbine Engine Technology. McGraw-Hill, New York, NY.
104. Turton, R. K. (1984). Principles of Turbomachinery. Spon, New York, NY.
105. U. S. Government Printing Office (1976). The U. S. Standard Atmosphere. Washington, D. C.
106. Van den Hout, F., and Koullen, J. (1997). A tiny turbojet for model aircraft. Mechanical Engineering. 119 (8), 66-69.
107. Vavra, M. H. (1974). Aero-Thermodynamics and Flow in Turbomachines. Krieger, New York, NY.
108. Wallis, R. A. (1983). Axial Flow Fans and Ducts. Wiley, New York, NY.
109. Wark, K., and Richards, D. (1999). Thermodynamics. McGraw-Hill, New York, NY.
110. Whittle, Sir F. (1981). Gas Turbine Aero-thermodynamics. Pergamon Press, Oxford, UK.
111. Wiesner, F. J. (1967). Areviewof slip factors for centrifugal impellers. ASME Transactions, Journal of Engineering for Power. 89, 558-572.
112. Wilson, D. G. (1982). Turbomachinery-From paddle wheels to turbojets. Mechanical Engineering. 104 (10), 28-40.
113. Wilson, D. G. (1984). The Design of High Efficiency Turbomachinery and Gas Turbines. MIT Press, Cambridge, MA.
114. Zucrow, M. J., and Hoffman, J. D. (1976). Gas Dynamics, Vols. 1 and 2. Wiley, New York, NY.
115. Aviation Week & Space Technology Flight International.
116. www.cfm56. com/.
117. www.enginealliance. com/.
118. www.geae. com/.
119. www.gepower. com/dhtml/aeroenergy/en us/.
120. www.pratt-whitney. com/.
121. www.pwc. ca.
122. www.rolls-royce. com/.
123. www.snecma-moteurs. com/.
124. www.V2500. com/.
125. www.jet-engine. net.