561
Index
A
Abott, I.H., 49
Active force, 8
Adachi, T., 128, 129
Adams, T., 269
Aero-derivative gas turbine, 376
Angle of attack, 49
Angle of incidence, 61
Aungier, R.H., 125, 126, 129
Axial chord, 72
B
Baehr, H.D., 393, 396
Balje, O.E., 240, 260, 519
Bernoulli’s work equation, 8
Blade
backward curved blades, 34, 35, 104
forward curved blades, 35, 104
radial end blades, 104
splitter blades, 511
Blade passage shock, 495
Blade speed, 3, 15
Blade-to-blade surfaces, 481
Bleier, F.P., 145
Blower, 97
Booster, 429
Boundary layer
boundary layer separation, 52−55
controlled boundary layer, 544
Bowing, 232
Bow shock, 494
Brennen, C.E., 285
Bypass turbojet, 428
© Springer Science+Business Media Dordrecht 2015
E. Dick, Fundamentals of Turbomachines, Fluid Mechanics and Its Applications 109,
DOI 10.1007/978-94-017-9627-9
C
Casarosa, C., 414
Casey, M.V., 269
Casing treatment, 531
Cavitation, 283
attached cavitation, 285
implosion, 283
Chiesa, P., 396
Choking, 162, 497, 499, 502
Chord, 49
Coandă-effect, 125
Cohen, H., 377
Contra-rotating propellers, 429
Controlled diffusion aerofoil, 492
Cooling
convection cooling, 379
film cooling, 379
impingement cooling, 379
steam cooling, 407
Cordier line, 259
Core engine, 436
Critical pressure, 161
Critical state, 161
Cross-flow fans, 100
Cumpsty, N.A., 519, 526
D
Degree of reaction
action part, 23, 28
isentropic degree of reaction, 218
kinematic degree of reaction, 103, 218
pressure degree of reaction, 103
reaction part, 23, 28
thermodynamic degree of reaction, 218