-
1
-
-
85024539694
-
Résumé of transonic-compressor research at NACA Lewis Laboratory
-
July
-
Lieblein, S. and Johnson, I. A. Résumé of transonic-compressor research at NACA Lewis Laboratory. Trans. ASME, J. Engng for Power, Ser. A, July 1961, 83, 219-234.
-
(1961)
Trans. ASME, J. Engng for Power, Ser. A
, vol.83
, pp. 219-234
-
-
Lieblein, S.1
Johnson, I.A.2
-
2
-
-
84904281326
-
Streamline curvature computing procedures for fluid flow problems
-
Novak, R. A. Streamline curvature computing procedures for fluid flow problems. Trans. ASME, J. Engng for Power, Ser. A, 1967, 89, 478-490.
-
(1967)
Trans. ASME, J. Engng for Power, Ser. A
, vol.89
, pp. 478-490
-
-
Novak, R.A.1
-
3
-
-
0028011644
-
NASA/GE fan and compressor research accomplishments
-
October
-
Smith Jr, L. H. NASA/GE fan and compressor research accomplishments. Trans. ASME, J. Turbomachinery, October 1994, 116, 555-569.
-
(1994)
Trans. ASME, J. Turbomachinery
, vol.116
, pp. 555-569
-
-
Smith Jr., L.H.1
-
4
-
-
0020268756
-
Recent advances in the performance of high bypass ratio fans
-
ICAS 82-413 Seattle
-
Nicholas, D. J. and Freeman, C. Recent advances in the performance of high bypass ratio fans. ICAS 82-413. 13th Congress of ICAS, Seattle, 1982.
-
(1982)
13th Congress of ICAS
-
-
Nicholas, D.J.1
Freeman, C.2
-
5
-
-
0021455795
-
Experimental study of a high-through-flow transonic axial compressor stage
-
Wennerstrom, A. J. Experimental study of a high-through-flow transonic axial compressor stage. Trans. ASME, J. Turbomachinery, 1984, 106, 552-560.
-
(1984)
Trans. ASME, J. Turbomachinery
, vol.106
, pp. 552-560
-
-
Wennerstrom, A.J.1
-
6
-
-
84971498570
-
Low aspect ratio transonic rotors: Part 1-Baseline design and performance
-
Law, C. H. and Wadia, A. R. Low aspect ratio transonic rotors: Part 1-Baseline design and performance. Trans. ASME, J. Turbomachinery, 1993, 115, 218-225.
-
(1993)
Trans. ASME, J. Turbomachinery
, vol.115
, pp. 218-225
-
-
Law, C.H.1
Wadia, A.R.2
-
7
-
-
4243125711
-
An investigation of the effect of cascade area ratios on transonic compressor performance
-
Wadia, A. R. and Copenhaver, W. W. An investigation of the effect of cascade area ratios on transonic compressor performance. Trans. ASME, J. Turbomachinery, 1996, 118, 760-770.
-
(1996)
Trans. ASME, J. Turbomachinery
, vol.118
, pp. 760-770
-
-
Wadia, A.R.1
Copenhaver, W.W.2
-
8
-
-
0024751325
-
Low aspect ratio compressors: Why and what it means
-
Wennerstrom, A. J. Low aspect ratio compressors: why and what it means. Trans. ASME, J. Turbomachinery, 1989, 111, 357-365.
-
(1989)
Trans. ASME, J. Turbomachinery
, vol.111
, pp. 357-365
-
-
Wennerstrom, A.J.1
-
10
-
-
0019896990
-
An improved time-marching method for turbomachinery flow calculation
-
Denton, J. D. An improved time-marching method for turbomachinery flow calculation. ASME paper 82-GT-23, 1982.
-
(1982)
ASME Paper
, vol.82 GT-23
-
-
Denton, J.D.1
-
11
-
-
0021586064
-
Computation of viscous compressible flow in blade cascades using an implicit iterative replacement algorithm
-
Conference Publication 1984-3 (Mechanical Engineering Publications, London)
-
Dawes, W. N. Computation of viscous compressible flow in blade cascades using an implicit iterative replacement algorithm. In IMechE Conference on Computational Methods in Turbomachinery, 1984, Conference Publication 1984-3 (Mechanical Engineering Publications, London).
-
(1984)
IMechE Conference on Computational Methods in Turbomachinery
-
-
Dawes, W.N.1
-
12
-
-
85085668755
-
An implicit finite difference code for inviscid and viscous cascade flow
-
July
-
Steger, J. L., Pulliam, T. R. and Chima, R. V. An implicit finite difference code for inviscid and viscous cascade flow. AIAA paper 80-1427, July 1980.
-
(1980)
AIAA Paper
, vol.80-1427
-
-
Steger, J.L.1
Pulliam, T.R.2
Chima, R.V.3
-
13
-
-
0019898218
-
An inviscid-viscous interaction treatment to predict the blade-to-blade performance of axial compressors with leading-edge normal shock waves
-
Calvert, W. J. An inviscid-viscous interaction treatment to predict the blade-to-blade performance of axial compressors with leading-edge normal shock waves. ASME paper 82-GT-135, 1982.
-
(1982)
ASME Paper
, vol.82 GT-135
-
-
Calvert, W.J.1
-
14
-
-
85040303521
-
Application of an inviscid-viscous interaction method to transonic compressor cascades
-
Calvert, W. J. Application of an inviscid-viscous interaction method to transonic compressor cascades. AGARDCP-351 paper 2, 1983.
-
(1983)
AGARDCP-351 Paper
, vol.2
-
-
Calvert, W.J.1
-
15
-
-
0021855548
-
A quasi-three-dimensional calculation system for the flow within transonic compressor blade rows
-
Calvert, W. J. and Cinder, R. B. A quasi-three-dimensional calculation system for the flow within transonic compressor blade rows. ASME paper 85-GT-22, 1985.
-
(1985)
ASME Paper
, vol.85 GT-22
-
-
Calvert, W.J.1
Cinder, R.B.2
-
16
-
-
0022042975
-
A quasi-three-dimensional turbomachinery blade design system, Parts I and II
-
Jennions, I. K. and Stow, P. A quasi-three-dimensional turbomachinery blade design system, Parts I and II. Trans. ASME, J. Engng for Gas Turbines and Power, 1985, 107, 301-316.
-
(1985)
Trans. ASME, J. Engng for Gas Turbines and Power
, vol.107
, pp. 301-316
-
-
Jennions, I.K.1
Stow, P.2
-
19
-
-
33749707992
-
The accelerating pace of advancing aero engine technology
-
February
-
Coplin, J. F. The accelerating pace of advancing aero engine technology. Aerospace, February 1984, 11(2), 17-23.
-
(1984)
Aerospace
, vol.11
, Issue.2
, pp. 17-23
-
-
Coplin, J.F.1
-
20
-
-
0031341243
-
The use of cyclic variations in strut stagger to reduce coupled blade-vane-strut-pylon interaction and system losses
-
Parry, A. B. The use of cyclic variations in strut stagger to reduce coupled blade-vane-strut-pylon interaction and system losses. ASME paper 97-GT-470, 1997.
-
(1997)
ASME Paper
, vol.97 GT-470
-
-
Parry, A.B.1
-
22
-
-
0017866222
-
A new stage stacking technique for axial-flow compressor performance prediction
-
Howell, A. R. and Calvert, W. J. A new stage stacking technique for axial-flow compressor performance prediction. Trans. ASME, J. Engng for Power, 1978, 100, 698-703.
-
(1978)
Trans. ASME, J. Engng for Power
, vol.100
, pp. 698-703
-
-
Howell, A.R.1
Calvert, W.J.2
-
23
-
-
0346049472
-
An improved compressor performance prediction model
-
London, paper C423/007, Mechanical Engineering Publications, London
-
Wright, P. I. and Miller, D. C. An improved compressor performance prediction model. In Proceedings of IMechE Conference on Turbomachinery, London, 1991, paper C423/007, pp. 59-68 (Mechanical Engineering Publications, London).
-
(1991)
Proceedings of IMechE Conference on Turbomachinery
, pp. 59-68
-
-
Wright, P.I.1
Miller, D.C.2
-
24
-
-
17444425401
-
Through flow calculations in axial turbomachines
-
Hirsch, C. and Denton, J. D. Through flow calculations in axial turbomachines. AGARD Advisory Report 175, 1981.
-
(1981)
AGARD Advisory Report
, vol.175
-
-
Hirsch, C.1
Denton, J.D.2
-
25
-
-
0029109491
-
A new endwall model for axial compressor throughflow calculations
-
Dunham, J. A new endwall model for axial compressor throughflow calculations. Trans. ASME, J. Turbomachinery, 1995, 117, 533-540.
-
(1995)
Trans. ASME, J. Turbomachinery
, vol.117
, pp. 533-540
-
-
Dunham, J.1
-
26
-
-
2142826671
-
Application of modified loss and deviation correlations to transonic axial compressors
-
Cetin, M., et al. Application of modified loss and deviation correlations to transonic axial compressors. AGARD Report 745, 1987.
-
(1987)
AGARD Report
, vol.745
-
-
Cetin, M.1
-
27
-
-
0023437684
-
Viscous-inviscid analysis of transonic and low Reynolds number airfoils
-
Drela, M. and Giles, M. B. Viscous-inviscid analysis of transonic and low Reynolds number airfoils. Am. Inst. Aeronaut. Astronaut. J., 1987, 25(10), 1347-1355.
-
(1987)
Am. Inst. Aeronaut. Astronaut. J.
, vol.25
, Issue.10
, pp. 1347-1355
-
-
Drela, M.1
Giles, M.B.2
-
28
-
-
0024090602
-
Prediction of compressor cascade performance using a Navier-Stokes technique
-
Hobbs, D. E., Davis, R. L. and Weingold, H. D. Prediction of compressor cascade performance using a Navier-Stokes technique. Trans. ASME, J. Turbomachinery, 1988, 110, 520-531.
-
(1988)
Trans. ASME, J. Turbomachinery
, vol.110
, pp. 520-531
-
-
Hobbs, D.E.1
Davis, R.L.2
Weingold, H.D.3
-
29
-
-
33749741915
-
A numerical method for the analysis of 3D viscous compressible flow in a turbine cascade with and without dihedral
-
Dawes, W. N. A numerical method for the analysis of 3D viscous compressible flow in a turbine cascade with and without dihedral. ASME paper 86-GT-145, 1986.
-
(1986)
ASME Paper
, vol.86 GT-145
-
-
Dawes, W.N.1
-
30
-
-
0028155069
-
Advanced transonic fan design procedure based on a Navier-Stokes method
-
Rhie, C. M., et al. Advanced transonic fan design procedure based on a Navier-Stokes method. Trans. ASME, J. Turbomachinery, 1994, 116, 291-297.
-
(1994)
Trans. ASME, J. Turbomachinery
, vol.116
, pp. 291-297
-
-
Rhie, C.M.1
-
31
-
-
0031354780
-
Evaluation of a 3D viscous code for turbomachinery flows
-
Calvert, W. J., et al. Evaluation of a 3D viscous code for turbomachinery flows. ASME paper 97-GT-078, 1997.
-
(1997)
ASME Paper
, vol.97 GT-078
-
-
Calvert, W.J.1
-
32
-
-
84997638205
-
Preliminary findings in certification of ADPAC
-
Barber, T. J., et al. Preliminary findings in certification of ADPAC. AIAA paper 94-2240, 1994.
-
AIAA Paper
, vol.94-2240
, pp. 1994
-
-
Barber, T.J.1
-
33
-
-
33749788718
-
-
Unpublished presentation at ASME Turbo Expo '94, The Hague, The Netherlands
-
Wisler, D. C. CFD code assessment in turbomachinery. Unpublished presentation at ASME Turbo Expo '94, The Hague, The Netherlands, 1994.
-
(1994)
CFD Code Assessment in Turbomachinery
-
-
Wisler, D.C.1
-
34
-
-
0141778711
-
Lessons from Rotor 37
-
Beijing
-
Denton, J. D. Lessons from Rotor 37. 3rd ISAIF Meeting, Beijing, 1996.
-
(1996)
3rd ISAIF Meeting
-
-
Denton, J.D.1
-
35
-
-
10244265267
-
CFD validation for propulsion system components
-
Dunham, J. CFD validation for propulsion system components. AGARD Advisory Report 355, 1998.
-
(1998)
AGARD Advisory Report
, vol.355
-
-
Dunham, J.1
-
36
-
-
0029163975
-
The effect of adding roughness and thickness to a transonic axial compressor rotor
-
October
-
Suder, K. L., Chima, R. V., Strazisar, A. J. and Roberts, W. B. The effect of adding roughness and thickness to a transonic axial compressor rotor. Trans. ASME, J. Turbomachinery, October 1995, 117, 491-505.
-
(1995)
Trans. ASME, J. Turbomachinery
, vol.117
, pp. 491-505
-
-
Suder, K.L.1
Chima, R.V.2
Strazisar, A.J.3
Roberts, W.B.4
-
39
-
-
0031703050
-
Analysis of aspect ratio effects on transonic rotor performance using a 3D viscous solver
-
Buchanan, C. R., Emmerson, P. R. and Spruce, M. Analysis of aspect ratio effects on transonic rotor performance using a 3D viscous solver. ASME paper 98-GT-250, 1998.
-
(1998)
ASME Paper
, vol.98 GT-250
-
-
Buchanan, C.R.1
Emmerson, P.R.2
Spruce, M.3
-
40
-
-
0031340590
-
The effect of hub leakage flow on two high speed axial flow compressor rotors
-
Shabbir, A., et al. The effect of hub leakage flow on two high speed axial flow compressor rotors. ASME paper 97-GT-346, 1997.
-
(1997)
ASME Paper
, vol.97 GT-346
-
-
Shabbir, A.1
-
41
-
-
0031340739
-
Effect of a mismatch between the buttons of variable stator vanes and the flowpath in a highly loaded transonic compressor stage
-
Escuret, J., et al. Effect of a mismatch between the buttons of variable stator vanes and the flowpath in a highly loaded transonic compressor stage. ASME paper 97-GT-471,1997.
-
(1997)
ASME Paper
, vol.97 GT-471
-
-
Escuret, J.1
-
43
-
-
0024866542
-
A method for the prediction of supersonic compressor blade performance
-
Freeman, C. and Cumpsty, N. A. A method for the prediction of supersonic compressor blade performance. ASME paper 89-GT-326, 1989.
-
(1989)
ASME Paper
, vol.89 GT-326
-
-
Freeman, C.1
Cumpsty, N.A.2
-
44
-
-
0027677224
-
Loss mechanisms in turbomachines
-
ASME Scholar Lecture.
-
Denton, J. D. Loss mechanisms in turbomachines. ASME Scholar Lecture. Trans. ASME, J. Turbomachinery, 1993, 115, 621-656.
-
(1993)
Trans. ASME, J. Turbomachinery
, vol.115
, pp. 621-656
-
-
Denton, J.D.1
-
45
-
-
0023572550
-
Performance of a civil fan rotor designed using a quasi-3D calculation system
-
Conference Publication 1987-6, paper C257/87 (Mechanical Engineering Publications, London)
-
Culvert, W. J., Ginder, R. B. and Lewis, G. Performance of a civil fan rotor designed using a quasi-3D calculation system. In IMechE Conference on TurbomachineryEfficiency Prediction and Improvement, 1987, Conference Publication 1987-6, paper C257/87 (Mechanical Engineering Publications, London).
-
(1987)
IMechE Conference on TurbomachineryEfficiency Prediction and Improvement
-
-
Culvert, W.J.1
Ginder, R.B.2
Lewis, G.3
-
47
-
-
18744438058
-
Reduction of compressor stator endwall losses through the use of bowed stators
-
Weingold, H. D., et al. Reduction of compressor stator endwall losses through the use of bowed stators. ASME paper 95-GT-380, 1995.
-
(1995)
ASME Paper
, vol.95 GT-380
-
-
Weingold, H.D.1
|