Turbomachinery design and theory by Aijaz A. Khan

By Aijaz A. Khan

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6. Two primary points will be observed: first, that the main element is a rotor or runner carrying blades or vanes; and secondly, that the path of the fluid in the rotor may be substantially axial, substantially radial, or in some cases a combination of both. Turbomachines can further be classified as follows: Turbines: Machines that produce power by expansion of a continuously flowing fluid to a lower pressure or head. Pumps: Machines that increase the pressure or head of flowing fluid. Fans: Machines that impart only a small pressure-rise to a continuously flowing gas; usually the gas may be considered to be incompressible.

60. 61. 62. 63. 64. 65. 66. 67. 68. 69. 70. 71. 72. 73. 74. 75. 76. 77. 78. 79. 80. 81. 82. Copyright 2003 by Marcel Dekker, Inc. All Rights Reserved Bibliography 83. 84. 85. 86. 87. 88. 89. 90. 91. 92. 93. 94. 95. 96. 97. 98. 99. 100. 101. 102. 103. 104. 105. 106. 107. 108. 391 Mallinson, D. , Lewis, W. G. E. (1948). The part load performance of various gas turbine engine schemes. Inst. Mech. Eng. 159:198– 219. Mattingley, J. , Heiser, W. , Daley, D. H. (1987). Aircraft Engine Design. AIAA Education Series.

1950). Steam Turbines. McGraw-Hill. Cohen, H, White, E. M. (1943). The Theoretical Determination of the Threedimensional Flow in an Axial Compressor with Special Reference to Constant Reaction Blading. C. Report, 6842. Carmichael, A. D. (1958). Stall Propagation in Compressors. D. Thesis, Cambridge University. Carter, A. D. S. (1957). The Effect of Reynolds Number on the Performance of a Single-Stage Compressor. Aeronautical Research Council, R and M. 3184. Cocrell, D. , Markland, E. (1963). Review of incompressible diffuser flow.

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