-
1
-
-
0030935568
-
Boundary layer development in axial compressors and turbines
-
225-237, 426-444
-
Halstead, D.E., Wisler, D.C., Okiishi, T.H., Walker, G.J., Hodson, H.P. and Shin, H.-W. Boundary layer development in axial compressors and turbines: Parts 1-4. Trans. ASME, J. Turbomach., 1997, 119, 114-139, 225-237, 426-444.
-
(1997)
Trans. ASME, J. Turbomach.
, vol.119
, Issue.PARTS 1-4
, pp. 114-139
-
-
Halstead, D.E.1
Wisler, D.C.2
Okiishi, T.H.3
Walker, G.J.4
Hodson, H.P.5
Shin, H.-W.6
-
2
-
-
0042191822
-
Blade row interference effects in axial turbomachinery stages: Blade row interactions in low pressure turbines
-
Brussels, February
-
Hodson, H.P. Blade row interference effects in axial turbomachinery stages: blade row interactions in low pressure turbines. VKI Lecture, Brussels, February 1998.
-
(1998)
VKI Lecture
-
-
Hodson, H.P.1
-
3
-
-
0029671701
-
Computation and simulation of wake-generated unsteady pressure and boundary layers in cascades
-
Fan, S. and Lakshminarayana, B. Computation and simulation of wake-generated unsteady pressure and boundary layers in cascades, Parts 1-2. Trans. ASME, J. Turbomach., 1996, 118, 96-121.
-
(1996)
Trans. ASME, J. Turbomach.
, vol.118
, Issue.PARTS 1-2
, pp. 96-121
-
-
Fan, S.1
Lakshminarayana, B.2
-
4
-
-
0041691149
-
Blade row interference effects in axial turbomachinery stages
-
Brussels, February
-
Sharma, O. Blade row interference effects in axial turbomachinery stages. VKI Lecture, Brussels, February 1998.
-
(1998)
VKI Lecture
-
-
Sharma, O.1
-
7
-
-
0019070772
-
Natural transition of boundary layers. The effects of turbulence, pressure gradient and flow history
-
Abu-Ghannam, B. and Shaw, R. Natural transition of boundary layers. The effects of turbulence, pressure gradient and flow history. J. Mech. Engng Sci., 1980, 22, 213-228.
-
(1980)
J. Mech. Engng Sci.
, vol.22
, pp. 213-228
-
-
Abu-Ghannam, B.1
Shaw, R.2
-
8
-
-
0006690064
-
Transition modelling for turbomachinery flows
-
Coupland, J. Transition modelling for turbomachinery flows. ERCOFTAC Bull., 1995, 24, 5-8.
-
(1995)
ERCOFTAC Bull.
, vol.24
, pp. 5-8
-
-
Coupland, J.1
-
10
-
-
0009996755
-
On recent advances of a massively-parallel time-accurate Navier-Stokes solver for unsteady turbomachinery flow
-
Athens
-
Eulitz, F., Engel, K., Nürnberger, D., Schmidt, S. and Yamamoto, K. On recent advances of a massively-parallel time-accurate Navier-Stokes solver for unsteady turbomachinery flow. In Proceedings of ECCOMAS, Athens, 1998.
-
(1998)
Proceedings of ECCOMAS
-
-
Eulitz, F.1
Engel, K.2
Nürnberger, D.3
Schmidt, S.4
Yamamoto, K.5
-
15
-
-
0007715119
-
-
ASME 98-GT-23
-
Dorney, D.J., Sondak, D.L., Ciszmas, P.G.A., Saren, V.E. and Savin, N.M. Full-annulus simulations of airfoil clocking in a 1 1/2 stage axial compressor. ASME 98-GT-23, 1999.
-
(1999)
Full-Annulus Simulations of Airfoil Clocking in a 1 1/2 Stage Axial Compressor
-
-
Dorney, D.J.1
Sondak, D.L.2
Ciszmas, P.G.A.3
Saren, V.E.4
Savin, N.M.5
-
16
-
-
0030482675
-
Performance improvement through indexing of turbine airfoils: Part 1 - Experimental investigation
-
Huber, F.W., Johnson, P.D., Sharma, O.P., Staubach, J.B. and Gaddis, S.W. Performance improvement through indexing of turbine airfoils: Part 1-Experimental investigation. Trans. ASME, J. Turbomach., 1995, 118, 630-635.
-
(1995)
Trans. ASME, J. Turbomach.
, vol.118
, pp. 630-635
-
-
Huber, F.W.1
Johnson, P.D.2
Sharma, O.P.3
Staubach, J.B.4
Gaddis, S.W.5
-
17
-
-
2942757053
-
Approximative Riemann solvers, parameter vector and differences schemes
-
Roe, P. Approximative Riemann solvers, parameter vector and differences schemes. J. Comp. Physics, 1981, 43, 357-372.
-
(1981)
J. Comp. Physics
, vol.43
, pp. 357-372
-
-
Roe, P.1
-
18
-
-
2442433925
-
Towards the ultimate conservation difference scheme, a second order sequel to Godunov's method
-
van Leer, B. Towards the ultimate conservation difference scheme, a second order sequel to Godunov's method. J. Comp. Physics, 1979, 32, 101-136.
-
(1979)
J. Comp. Physics
, vol.32
, pp. 101-136
-
-
van Leer, B.1
-
19
-
-
0027558896
-
New two-grid acceleration method for unsteady Navier-Stokes calculations
-
He, L. New two-grid acceleration method for unsteady Navier-Stokes calculations. J. Propulsion and Power, 1993, 9, 272.
-
(1993)
J. Propulsion and Power
, vol.9
, pp. 272
-
-
He, L.1
-
20
-
-
0027560166
-
Quasi three dimensional nonreflecting boundary conditions for Euler equations calculations
-
Saxer, A.P. and Giles, M. Quasi three dimensional nonreflecting boundary conditions for Euler equations calculations. Am. Inst. Aeronaut. Astronaut. J. Propulsion and Power, 1993, 9(2), 263-271.
-
(1993)
Am. Inst. Aeronaut. Astronaut. J. Propulsion and Power
, vol.9
, Issue.2
, pp. 263-271
-
-
Saxer, A.P.1
Giles, M.2
-
23
-
-
0006694367
-
-
14th ICNMFD, Bangalore, India
-
Engel, K., Eulitz, F., Pokorny, S. and Faden, M. Validation of different TVD-schemes for the calculation of the unsteady turbomachinery flow. 14th ICNMFD, Bangalore, India, 1996.
-
(1996)
Validation of Different TVD-Schemes for the Calculation of the Unsteady Turbomachinery Flow
-
-
Engel, K.1
Eulitz, F.2
Pokorny, S.3
Faden, M.4
-
25
-
-
0034529388
-
Numerical and experimental investigation of unsteady flow interaction in a low-pressure multi-stage turbine
-
Höhn, W. and Heinig, K. Numerical and experimental investigation of unsteady flow interaction in a low-pressure multi-stage turbine. Trans. ASME J. Turbomach., 2000, 122, 628-633.
-
(2000)
Trans. ASME J. Turbomach.
, vol.122
, pp. 628-633
-
-
Höhn, W.1
Heinig, K.2
|