Short-duration facilities have been used for the past 35 years to obtain measurements of heat transfer, aerodynamic loading, vibratory response, film-cooling influence, purge flow migration, and aeroperformance for full-stage, high-pressure turbines operating at design-corrected conditions of flow function, corrected speed, and stage pressure ratio. This paper traces the development of experimental techniques now in use at The Ohio State University (OSU) Gas Turbine Laboratory (GTL) from initial work in this area at the Cornell Aeronautical Laboratory (CAL, later to become Calspan) from 1975 through to the present. It is intended to summarize the wide range of research that can be performed with a short-duration facility and highlight the types of measurements that are possible. Beginning with heat flux measurements for the vane and blade of a Garrett TFE 731-2 HP turbine stage with vane pressure-surface slot cooling, the challenge of each experimental program has been to provide data to aid turbine designers in understanding the relevant flow physics and help drive the advancement of predictive techniques. Through many different programs, this has involved collaborators at a variety of companies and experiments performed with turbine stages from Garrett, Allison, Teledyne, Pratt and Whitney (P/W), General Electric Aviation (GEA), Rocketdyne, Westinghouse, and Honeywell. The vane/blade interaction measurement and computational fluid dynamics (CFD) program, which ran from the early 1980s until 2000, provided a particularly good example of what can be achieved when experimentalists and computational specialists collaborate closely. Before conclusion of this program in 2000, the heat flux and pressure measurements made for this transonic turbine operated with and without vane trailing edge cooling flow were analyzed and compared to predictive codes in conjunction with engineers at Allison, United Technologies Research Center (UTRC), P/W, and GEA in jointly published papers. When the group moved to OSU in 1995 along with the facility used at Calspan, refined techniques were needed to meet new research challenges, such as investigating blade-damping and forced response, measuring aeroperformance for different configurations, and preparing for advanced cooling experiments that introduced complicating features of an actual engine to further challenge computational predictions. This required conversion of the test-gas heating method from a shock-tunnel approach to a blowdown approach using a combustor emulator to also create inlet temperature profiles, the development of instrumentation techniques to work with a thin-walled airfoil with backside cooling, and the adoption of experimental techniques that could be used to successfully operate fully cooled turbine stages (vane row-cooled, blade row-cooled, and proper cavity purge flow provided). Further, it was necessary to develop techniques for measuring the aeroperformance of these fully cooled machines.

References

References
1.
Dunn
,
M. G.
, and
Stoddard
,
F. J.
,
1977
, “
Application of Shock-Tube Technology to the Measurement of Heat-Transfer Rate to Gas Turbine Components
,”
Proceedings of the 11th International Symposium on Shock Tubes and Waves
,
Seattle, WA
, July 11–14.
2.
Dunn
,
M. G.
, and
Stoddard
,
F. J.
,
1977
, “
Measurement of Heat Transfer Rate to Gas Turbine Components
,”
Proceedings of the 11th International Symposium on Shock Tubes and Waves
,
Seattle, WA
, July 11–14.
3.
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Lotsof
,
J.
,
MacArthur
,
C. D.
, and
Cohrs
,
B.
,
1991
, “
Uncertainty Analysis of Turbine Aerodynamic Performance Measurements in Short Duration Test Facilities
,”
AIAA/SAE/ASME 27th Joint Propulsion Conference
, Sacramento, CA, June 24–26,
AIAA
Paper No. 91-2131.10.2514/6.1991-2131
4.
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
1998
, “
High-Accuracy Turbine Performance Measurements in Short-Duration Facilities
,”
ASME J. Turbomach.
,
120
, pp.
1
9
.10.1115/1.2841382
5.
Haldeman
,
C. W.
,
Dunn
,
M. G.
, and
Mathison
,
R. M.
,
2010
, “
Fully-Cooled Single Stage HP Transonic Turbine: Part I—Influence of Cooling Mass Flow Variations and Inlet Temperature Profiles on Blade Internal and External Aerodynamics
,”
ASME J. Turbomach.
,
134
(
3
), p.
031010
.10.1115/1.4002967
6.
Haldeman
,
C.
,
Dunn
,
M.
,
Mathison
,
R. M.
,
Troha
,
W.
,
Vander Hoek
,
T.
, and
Riahi
,
A.
,
2012
, “
Aeroperformance Measurements for a Fully Cooled High-Pressure Turbine Stage
,”
ASME
Paper No. GT2012-69941.
7.
Dunn
,
M. G.
,
1985
, “
Turbine Heat-Flux Measurements: Influence of Slot Injection on Vane Trailing Edge Heat Transfer and Influence of Rotor on Vane Heat Transfer
,”
ASME J. Eng. Power
,
107
, pp.
76
83
.10.1115/1.3239700
8.
Dunn
,
M. G.
, and
Chupp
,
R. E.
,
1989
, “
Influence of Vane/Blade Spacing and Cold-Gas Injection on Vane and Blade Heat-Flux Distributions for the Teledyne 702 HP Turbine Stage
,”
J. Propul. Power
,
5
(
2
), pp.
212
220
.10.2514/3.23138
9.
Haldeman
,
C. W.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2004
, “
Design, Construction and Operation of a Combustor Emulator for Short-Duration High-Pressure Turbine Experiments
,”
AIAA Joint Propulsion Conference
,
Ft. Lauderdale, FL
, July 11–14,
AIAA
Paper No. 2004-3829.10.2514/6.2004-3829
10.
Haldeman
,
C.
,
1989
, “
An Experimental Study of Radial Temperature Profile Effects on Turbine Tip Shroud Heat-Transfer
,” Master's thesis, MIT, Cambridge, MA.
11.
Winstanley
,
D. K.
,
Booth
,
T. C.
, and
Dunn
,
M. G.
,
1981
, “
The Predictability of Turbine Vane Convection Heat Transfer
,”
17th Joint Propulsion Conference AIAA/ASME/SAE
,
Colorado Springs, CO
, July 27–29,
AIAA
Paper No. 81-1435.10.2514/6.1981-1435
12.
Dunn
,
M. G.
, and
Hause
,
A.
,
1982
, “
Measurement of Heat Flux and Pressure in a Turbine Stage
,”
ASME J. Eng. Power
,
104
(
1
), pp.
215
223
.10.1115/1.3227253
13.
Dunn
,
M. G.
,
Rae
,
W. J.
, and
Holt
,
J. L.
,
1984
, “
Measurement and Analysis of Heat Flux Data in a Turbine Stage: Part I—Description of Experimental Apparatus and Data Analysis
,”
ASME J. Eng. Power
,
106
, pp.
229
233
.10.1115/1.3239539
14.
Dunn
,
M. G.
,
Rae
,
W. J.
, and
Holt
,
J. L.
,
1984
, “
Measurement and Analysis of Heat Flux Data in a Turbine Stage: Part II—Discussion of Results and Comparison with Predictions
,”
ASME J. Eng. Power
,
106
, pp.
234
240
.10.1115/1.3239540
15.
Dunn
,
M. G.
,
Lukis
,
G.
,
Urso
,
M.
,
Hiemenz
,
R. J.
,
Orszulak
,
R. L.
, and
Kay
,
N. J.
,
1984
, “
Instrumentation for Gas Turbine Research in Short-Duration Facilities
,”
SAE
Technical Paper 841504.10.4271/841504
16.
Rivir
,
R. B.
,
Elrod
,
W. C.
, and
Dunn
,
M. G.
,
1985
, “
Two Spot Laser Velocimeter Measurements of Velocity and Turbulence Intensity in Shock Tube Driven Turbine Flows
,” AGARD-CPP-390, Paper No. 33.
17.
Dunn
,
M. G.
,
1986
, “
Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part 1—Time-Averaged Results
,”
ASME J. Turbomach.
,
108
, pp.
90
97
.10.1115/1.3262029
18.
Dunn
,
M. G.
,
George
,
W. K.
,
Rae
,
W. J.
,
Woodward
,
S. H.
,
Moller
,
J. C.
, and
Seymour
,
P. J.
,
1986
, “
Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part II—Description of Analysis Technique and Typical Time-Resolved Measurements
,”
ASME J. Turbomach.
,
108
, pp.
98
107
.10.1115/1.3262030
19.
Rae
,
W. J.
,
Taulbee
,
D. B.
,
Civinskas
,
K. C.
, and
Dunn
,
M. G.
,
1986
, “
Turbine-Stage Heat Transfer: Comparison of Short-Duration Measurements With State-of-the-Art Prediction
,”
AIAA
Paper No. 86-1465.10.2514/6.1986-1465
20.
Taulbee
,
D. B.
,
Tran
,
L. T.
, and
Dunn
,
M. G.
,
1988
, “
Stagnation Point and Surface Heat Transfer for a Turbine Stage: Prediction and Comparison With Data
,”
Gas Turbine and Aeroengine Congress and Exhibition
,
Amsterdam, The Netherlands
, June 6–9,
ASME
Paper No. 88-GT-30.
21.
Dunn
,
M. G.
,
Martin
,
H. L.
, and
Stanek
,
M. J.
,
1986
, “
Heat-Flux and Pressure Measurements and Comparison With Prediction for a Low Aspect Ratio Turbine Stage
,”
31st ASME International Gas Turbine Conference
,
Dusseldorf, Germany
, June 8–12.
22.
Dunn
,
M. G.
, and
Chupp
,
R. E.
,
1988
, “
Time-Averaged Heat-Flux Distributions and Comparison With Prediction for the Teledyne 702 HP Turbine Stage
,”
ASME J. Eng. Power
,
110
, pp.
51
56
.10.1115/1.3240086
23.
Guenette
,
G. R.
,
Epstein
,
A. H.
, and
Ito
,
E.
,
1989
, “
Turbine Aerodynamic Performance Measurements in Short Duration Facilities
,”
AIAA
Paper No. 89-2690.10.2514/6.1989-2690
24.
Kahveci
,
H. S.
,
Haldeman
,
C. W.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2011
, “
Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part I—Experimental Configuration and Data Review With Inlet Temperature Profile Effects
,” ASME TurboExpo, Vancouver, Canada, June 6–10,
ASME
Paper No. GT2011-46570.10.1115/GT2011-46570
25.
Dunn
,
M. G.
,
Seymour
,
P. J.
,
Woodward
,
S. H.
,
George
,
W. K.
, and
Chupp
,
R. E.
,
1989
, “
Phase Resolved Heat-Flux Measurements on a Blade of a Full-Scale Rotating Turbine
,”
ASME J. Turbomach.
,
111
, pp.
8
19
.10.1115/1.3262242
26.
Dunn
,
M. G.
,
1990
, “
Phase and Time-Resolved Measurements of Unsteady Heat Transfer and Pressure in a Full-Stage Rotating Turbine
,”
ASME J. Turbomach.
,
112
, pp.
531
538
.10.1115/1.2927691
27.
Metzger
,
D. E.
,
Dunn
,
M. G.
, and
Hah
,
C.
,
1990
, “
Turbine Tip and Shroud Heat Transfer
,”
ASME
Paper No. 90-GT-333.
28.
Rao
,
K. V.
,
Delaney
,
R. A.
, and
Dunn
,
M. G.
,
1990
, “
Investigation of Unsteady Flow Through Transonic Turbine Stage—Part I: Analysis
,”
26th Joint Propulsion Conference
,
Orlando, FL
, July 16–18,
AIAA
Paper No. 90-2408.10.2514/6.1990-2408
29.
Dunn
,
M. G.
,
Bennett
,
W. A.
,
Delaney
,
R. A.
, and
Rao
,
K. V.
,
1990
, “
Investigation of Unsteady Flow Through a Transonic Turbine Stage—Part II: Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data
,”
26th Joint Propulsion Conference
,
Orlando, FL
, July 16–18,
AIAA
Paper No. 90-2409.10.2514/6.1990-2409
30.
Rao
,
K. V.
,
Delaney
,
R. A.
, and
Dunn
,
M. G.
,
1994
, “
Vane-Blade Interaction in a Transonic Turbine: Part I—Aerodynamics
,”
J. Propul. Power
,
10
(
3
), pp.
305
311
.10.2514/3.23757
31.
Rao
,
K. V.
,
Delaney
,
R. A.
, and
Dunn
,
M. G.
,
1994
, “
Vane-Blade Interaction in a Transonic Turbine: Part II—Heat Transfer
,”
J Propul. Power
,
10
(
3
), pp.
312
317
.10.2514/3.23758
32.
Davis
,
R. L.
,
Shang
,
T.
,
Buteau
,
J.
, and
Ni
,
R. H.
,
1996
, “
Prediction of 3-D Unsteady Flow in Multi-Stage Turbomachinery Using an Implicit Dual Time-Step Approach
,”
AIAA
Paper No. 96-2565.10.2514/6.1996-2565
33.
Giles
,
M. B.
, and
Haimes
,
R.
,
1993
, “
Validation of a Numerical Method for Unsteady Flow Calculations
,”
ASME J. Turbomach.
,
115
, pp.
110
117
.10.1115/1.2929195
34.
Dorney
,
D.
, and
Davis
,
R.
,
1992
, “
Navier-Stokes Analysis of Turbine Blade Heat Transfer and Performance
,”
ASME J. Turbomach.
,
114
, pp.
795
806
.10.1115/1.2928033
35.
Venable
,
B. L.
,
Delaney
,
R. A.
,
Busby
,
J. A.
,
Davis
,
R. L.
,
Dorney
,
D. J.
,
Dunn
,
M. G.
,
Haldeman
,
C. W.
, and
Abhari
,
R. S.
,
1999
, “
Influence of Vane-Blade Spacing on Transonic Turbine Stage Aerodynamics: Part I—Time-Averaged Data and Analysis
,”
ASME J. Turbomach.
,
121
, pp.
663
672
.10.1115/1.2836718
36.
Busby
,
J. A.
,
Davis
,
R. L.
,
Dorney
,
D. J.
,
Dunn
,
M. G.
,
Haldeman
,
C. W.
,
Abhari
,
R. S.
,
Venable
,
B. L.
, and
Delaney
,
R. A.
,
1999
, “
Influence of Vane-Blade Spacing on Transonic Turbine Stage Aerodynamics: Part II—Time-Resolved Data and Analysis
,”
ASME J. Turbomach.
,
121
, pp.
673
682
.10.1115/1.2836719
37.
Barter
,
J. W.
,
Vitt
,
P. H.
, and
Chen
,
J. P.
,
2000
, “
Interation Effects in a Transonic Turbine Stage
,” ASME Turbo Expo, Munich, Germany, May 8–11,
ASME
Paper No. 2000-GT-0376.
38.
Dunn
,
M. G.
,
Haldeman
,
C. W.
,
Abhari
,
R. S.
, and
McMillan
,
M. L.
,
2000
, “
Influence of Vane-Blade Spacing on the Time-Averaged Heat Flux for a Transonic Turbine
,”
ASME J. Turbomach.
,
122
, pp.
684
691
.10.1115/1.1313818
39.
Giles
,
M. B.
,
1988
, “
UNSFLO: A Numerical Method for Unsteady Inviscid Flow in Turbomachinery
,” MIT Gas Turbine Laboratory Report No. 195.
40.
Giles
,
M.
, and
Haimes
,
R.
,
1993
, “
Validation of a Numerical Method for Unsteady Flow Calculations
,”
ASME J. Turbomach.
,
115
, pp.
110
117
.10.1115/1.2929195
41.
Abhari
,
R. S.
,
Guenette
,
G. R.
,
Epstein
,
A. H.
, and
Giles
,
M. B.
,
1992
, “
Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations
,”
ASME J. Turbomach.
,
114
, pp.
818
827
.10.1115/1.2928035
42.
Dunn
,
M.
, and
Haldeman
,
C.
,
2000
, “
Time-Averaged Heat Flux for a Recessed Tip, Lip and Platform of a Transonic Turbine Blade
,”
ASME J. Turbomach.
,
122
, pp.
692
698
.10.1115/1.1311285
43.
Dunn
,
M. G.
,
Kim
,
J.
,
Civinskas
,
K. C.
, and
Boyle
,
R. J.
,
1994
, “
Time-Averaged Heat Transfer and Pressure Measurements and Comparison With Predictions for a Two-Stage Turbine
,”
ASME J. Turbomach.
,
116
(
1
), pp.
14
22
.10.1115/1.2928270
44.
Dunn
,
M. G.
, and
Haldeman
,
C. W.
,
1995
, “
Phase-Resolved Surface Pressure and Heat-Transfer Measurements on the Blade of a Two-Stage Turbine
,”
ASME J. Fluids Eng.
,
117
, pp.
653
658
.10.1115/1.2817318
45.
Dunn
,
M. G.
, and
Kim
,
J.
,
1995
, “
Turbine Blade Platform, Blade Tip and Shroud Heat Transfer
,” 12th International Symposium for Airbreathing Engines, Melbourne, Australia, September 10–15.
46.
Dunn
,
M. G.
,
Kim
,
J.
, and
Rae
,
W. J.
,
1997
, “
Investigation of the Heat-Island Effect for Heat-Flux Measurements in Short-Duration Facilities
,”
ASME J. Turbomach.
,
119
, pp.
753
760
.10.1115/1.2841185
47.
Bergholz
,
R. F.
,
Dunn
,
M. G.
, and
Steuber
,
G. D.
,
2000
, “
Rotor/Stator Heat Transfer Measurements and CFD Predictions for Short-Duration Turbine Rig Tests
,”
45th International Gas Turbine Conference
,
Munich, Germany
, May 8–11,
ASME
Paper No. 2000-GT-0208.
48.
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2004
, “
Heat Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage
,”
ASME J. Turbomach.
,
126
, pp.
101
109
.10.1115/1.1626132
49.
Clark
,
J. P.
,
Stetson
,
G. M.
,
Magge
,
S. S.
,
Ni
,
R. H.
,
Haldeman
,
C. W.
, Jr.
, and
Dunn
,
M. G.
,
2000
, “
The Effect of Airfoil Scaling on the Predicted Unsteady Loading on the Blade of a 1 and 1/2 Stage Transonic Turbine and a Comparison With Experimental Results
,” 45th International Gas Turbine Conference, Munich, Germany, May 8–11,
ASME
Paper No. 2000-GT-0446.
50.
Davis
,
R. L.
,
Yao
,
J.
,
Clark
,
J. P.
,
Stetson
,
G.
,
Alonso
,
J. J.
,
Jameson
,
A.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2002
, “
Unsteady Interaction Between a Transonic Turbine Stage and Downstream Components
,”
ASME
Paper No. GT-2002-30364.
51.
Green
,
B. R.
,
Barter
,
J. W.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2005
, “
Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results
,”
ASME J. Turbomach.
,
127
, pp.
736
746
.10.1115/1.1934410
52.
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Barter
,
J. W.
,
Green
,
B. R.
, and
Bergholz
,
R. F.
,
2005
, “
Aerodynamic and Heat-Flux Measurements With Predictions on a Modern One and 1/2 Stage High Pressure Turbine
,”
ASME J. Turbomach.
,
127
, pp.
522
531
.10.1115/1.1861916
53.
Molter
,
S.
,
Dunn
,
M. G.
,
Haldeman
,
C. W.
,
Bergholz
,
R. F.
, and
Vitt
,
P.
,
2006
, “
Heat-Flux Measurements and Predictions for the Blade Tip Region of a High-Pressure Turbine
,” ASME Turbo Expo, Barcelona, Spain, May 8–11,
ASME
Paper No. GT2006-90048.10.1115/GT2006-90048
54.
Crosh
,
E. A.
,
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Holmes
,
D. G.
, and
Mitchell
,
B. E.
,
2010
, “
Investigation of Turbine Shroud Distortions on the Aerodynamics of a One and One-Half Stage High-Pressure Turbine
,”
ASME J. Turbomach.
,
133
(
3
), p.
031002
.10.1115/1.4001176
55.
Tallman
,
J. A.
,
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Tolpadi
,
A. K.
, and
Bergholz
,
R. F.
,
2009
, “
Heat Transfer Measurements and Predictions for a Modern, High-Pressure Transonic Turbine, Including Endwalls
,”
ASME J. Turbomach.
,
131
(
2
), p.
021001
.10.1115/1.2985072
56.
Haldeman
,
C. W.
,
Mathison
,
R. M.
,
Dunn
,
M. G.
,
Southworth
,
S.
,
Harral
,
J. W.
, and
Heitland
,
G.
,
2008
, “
Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine—Part I: Experimental Approach
,”
ASME J. Turbomach.
,
130
(
2
), p.
021015
.10.1115/1.2750676
57.
Haldeman
,
C. W.
,
Mathison
,
R. M.
,
Dunn
,
M. G.
,
Southworth
,
S.
,
Harral
,
J. W.
, and
Heitland
,
G.
,
2008
, “
Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine—Part II: Experimental Results
,”
ASME J. Turbomach.
,
130
(
2
), p.
021016
.10.1115/1.2750678
58.
Guenette
,
G. R.
,
Epstein
,
A. H.
,
Giles
,
M. B.
,
Hanes
,
R.
, and
Norton
,
R. J. G.
,
1989
, “
Fully Scaled Transonic Turbine Rotor Heat Transfer Measurements
,”
ASME J. Turbomach.
,
111
, pp.
1
7
.10.1115/1.3262231
59.
Abhari
,
R. S.
,
Guenette
,
G. R.
,
Epstein
,
A. H.
, and
Giles
,
M. B.
,
1991
, “
Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculation
,” ASME Paper No. 91-GT-268.
60.
Southworth
,
S.
,
Dunn
,
M. G.
,
Haldeman
,
C. W.
,
Chen
,
J. P.
,
Heitland
,
G.
, and
Liu
,
J.
,
2009
, “
Time-Accurate Predictions for a Fully Cooled High-Pressure Turbine Stage: Part I—Comparison of Predictions With Data
,”
ASME J. Turbomach.
,
131
(
3
), p.
031003
.10.1115/1.2985075
61.
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Southworth
,
S. A.
,
Chen
,
J.-P.
,
Heitland
,
G.
, and
Liu
,
J.
,
2009
, “
Time-Accurate Predictions for a Fully Cooled High-Pressure Turbine Stage: Part II—Methodology for Quantifications of Prediction Quality
,”
ASME J. Turbomach.
,
131
, p.
031004
.10.1115/1.2985076
62.
Haldeman
,
C. W.
,
Dunn
,
M. G.
, and
Mathison
,
R. M.
,
2010
, “
Fully-Cooled Single Stage HP Transonic Turbine: Part II—Influence of Cooling Mass Flow Changes and Inlet Temperature Profiles on Blade and Shroud Heat-Transfer
,”
ASME J. Turbomach.
,
134
(
3
), p.
031011
.10.1115/1.4002968
63.
Mathison
,
R. M.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part I—Vane Inlet Temperature Profile Generation and Migration
,”
ASME J. Turbomach.
,
134
(
1
), p.
011006
.10.1115/1.4002994
64.
Mathison
,
R. M.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part II—Influence of Inlet Temperature Profile on Blade Heat Flux
,”
ASME J. Turbomach.
,
134
(
1
), p.
011007
.10.1115/1.4002995
65.
Mathison
,
R. M.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part III—Impact of Hot Streak Characteristics on Blade Row Heat Flux
,”
ASME J. Turbomach.
,
134
(
1
), p.
011008
.10.1115/1.4002996
66.
Mathison
,
R. M.
,
Wishart
,
M. B.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Temperature Predictions and Comparison With Measurements for the Blade Leading Edge and Platform of a 1-1/2 Stage Transonic HP Turbine
,”
ASME J. Turbomach.
,
134
(
1
), p.
011016
.10.1115/1.4002992
67.
Kahveci
,
H. S.
,
Haldeman
,
C. W.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2011
, “
Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part II—Effect of Cooling Variation on Vane Airfoil and Inner Endwall
,” ASME Turbo Expo, Vancouver, Canada,
ASME
Paper No. GT2011-46573.10.1115/GT2011-46573
68.
Mathison
,
R. M.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Heat Transfer for the Blade of a Cooled Stage and One-Half High-Pressure Turbine: Part I—Influence of Vane Cooling and Disk Cavity Purge Flow
,”
ASME J. Turbomach.
,
134
(
3
), p.
031014
.10.1115/1.4003173
69.
Mathison
,
R. M.
,
Haldeman
,
C. W.
, and
Dunn
,
M. G.
,
2010
, “
Heat Transfer for the Blade of a Cooled One and One-Half Stage High-Pressure Turbine: Part II–Influence of Purge Cooling Variation
,”
ASME J. Turbomach.
,
134
(
3
), p.
031015
.10.1115/1.4003174
70.
Green
,
B. R.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2012
, “
Comparison of Harmonic and Time Marching Unsteady CFD Solutions With Measurements for a Single Stage High-Pressure Turbine
,”
ASME
Paper No. GT2012-69934.
71.
Green
,
B. R.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2012
, “
Time-Averaged and Time-Accurate Aerodynamics Effects of Forward Rotor Cavity Purge Flow for a High-Pressure Turbine: Part I—Analytical and Experimental Comparisons
,”
ASME
Paper No. GT2012-69937.
72.
Green
,
B. R.
,
Mathison
,
R. M.
, and
Dunn
,
M. G.
,
2012
, “
Time-Averaged and Time-Accurate Aerodynamic Effects of Rotor Purge Flow for a Modern, One and One-Half Stage High-Pressure Turbine: Part II—Analytical Flow Field Analysis
,” ASME Paper No. GT2012-69939.
73.
Jouini
,
D. B. M.
,
Little
,
D.
,
Bancalari
,
E.
,
Dunn
,
M. G.
,
Haldeman
,
C. W.
, and
Johnson
P. D.
,
2003
, “
Experimental Investigation of Airfoil Wake Clocking Impacts on Aerodynamic Performance in a Two Stage Turbine Test Rig
,”
ASME
Paper No. GT2003-38872.10.1115/GT2003-38872
74.
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Barter
,
J. W.
,
Green
,
B. R.
, and
Bergholz
,
R. F.
,
2005
, “
Experimental Investigation Of Vane Clocking in a One and 1/2 Stage High Pressure Turbine
,”
ASME J. Turbomach.
,
127
, pp.
512
521
.10.1115/1.1861915
75.
Haldeman
,
C. W.
,
Krumanaker
,
M. L.
, and
Dunn
,
M. G.
,
2003
, “
Influence of Clocking and Vane/Blade Spacing on the Unsteady Surface Pressure Loading for a Modern Stage and One-Half Transonic Turbine
,”
ASME J. Turbomach.
,
125
, pp.
743
753
.10.1115/1.1625398
76.
Haldeman
,
C. W.
,
Dunn
,
M. G.
,
Abhari
,
R. S.
,
Johnson
,
P. D.
, and
Montesdeoca
,
X. A.
,
2000
, “
Experimental and Computational Investigation of the Time-Averaged and Time-Resolved Pressure Loading on a Vaneless Counter-Rotating Turbine
,”
45th International Gas Turbine Conference
,
Munich, Germany
, May 8–11,
ASME
Paper No. 2000-GT-0445.
77.
Weaver
,
M. W.
,
Manwaring
,
S.
,
Abhari
,
R. S.
,
Dunn
,
M. G.
,
Salay
,
M. J.
,
Frey
,
K. K.
, and
Heidegger
,
N.
,
2000
, “
Forcing Function Measurements and Predictions of a Transonic Vaneless Counter-Rotating Turbine
,” ASME Paper No. 2000-GT-0375.
78.
Kielb
,
J. J.
, and
Abhari
,
R. S.
,
2001
, “
Experimental Study of Aerodynamic and Structural Damping in a Full-Scale Rotating Turbine
,” ASME Paper No. 2001-GT-0262.
79.
Kielb
,
J. J.
,
Abhari
,
R. S.
, and
Dunn
,
M. G.
,
2001
, “
Experimental and Numerical Study of Forced Response in a Full-Scale Rotating Turbine
,” ASME Turbo Expo, New Orleans, LA, June 4–7,
ASME
Paper No. 2001-GT-0263.
80.
Panovsky
,
J.
,
Liu
,
J.
, and
Bakhle
,
M. A.
,
2002
, “
Comparisons of Experimental and Computational Forced Response in a High Pressure Turbine
,”
7th National Turbine Engine High Cycle Fatigue Conference
, Palm Beach, FL, May 14–17.
You do not currently have access to this content.