-
1
-
-
13544253990
-
Results of a blind companion of wind turbine model predictions to measurements of nrel’s unsteady aerodynamics experiment in the nasa ames wind tunnel
-
tin Review, Report. National Renewable Energy Laboratory Golden. CO
-
Simms, D., Schreck, S., Hand, M., and Fingersh, L., tin Review, “Results of a Blind Companion of Wind Turbine Model Predictions to Measurements of NREL’s Unsteady Aerodynamics Experiment in the NASA Ames Wind Tunnel.” NREL Tech. Report. National Renewable Energy Laboratory Golden. CO.
-
NREL Tech
-
-
Simms, D.1
Schreck, S.2
Hand, M.3
Fingersh, L.4
-
2
-
-
0017368814
-
Some current research m unsteady fluid dynamics-the 1976 freeman scholar- lecture
-
McCroskey, W. J., 1977, “Some Current Research m Unsteady Fluid Dynamics-The 1976 Freeman Scholar- Lecture.” ASME J. Fluids Eng., 99. No. 1, pp. 8-39.
-
(1977)
ASME J. Fluids Eng.
, vol.99
, Issue.1
, pp. 8-39
-
-
McCroskey, W.J.1
-
3
-
-
0023834009
-
Progress m analysis and prediction of dynamic stall
-
Carr, L. W., 1988, “Progress m Analysis and Prediction of Dynamic Stall,” J. of Aircraft. 25. No. 1, pp. 6-17.
-
(1988)
J. Of Aircraft
, vol.25
, Issue.1
, pp. 6-17
-
-
Carr, L.W.1
-
4
-
-
27744504516
-
Dynamic stall on wind turbine blades
-
Golden CO
-
Butterfield, C., Hansen, A., Simms, D., and Scott, G., 1991, “Dynamic Stall on Wind Turbine Blades”.NREL TP-257-4510, National Renewable Energy Laboratory. Golden CO.
-
(1991)
NREL TP-257-4510, National Renewable Energy Laboratory
-
-
Butterfield, C.1
Hansen, A.2
Simms, D.3
Scott, G.4
-
5
-
-
0005654512
-
-
NREL TP-441-7080. National Renewable Energy Laboratory. Golden. CO
-
Shipley, D., Miller, M., Robinson, M., Luttges, M., and Sunms, D., 1994. “Evidence that Aerodynamic Effects. Including Dynamic StalL Dictate HAWT Structure Loads and Power Generation in Highly Transient Tune Frames.” NREL TP-441-7080. National Renewable Energy Laboratory. Golden. CO.
-
(1994)
Evidence that Aerodynamic Effects. Including Dynamic Stall Dictate HAWT Structure Loads and Power Generation in Highly Transient Tune Frames.
-
-
Shipley, D.1
Miller, M.2
Robinson, M.3
Luttges, M.4
Sunms, D.5
-
6
-
-
0346010339
-
-
NREL TP-442-6912, National Renewable Energy Lab., Golden CO
-
Shipley, D., Miller, M., and Robinson, M., 1995. “Dynamic Stall Occurrence on a Horizontal Axis Wind Turbine Blade.” NREL TP-442-6912, National Renewable Energy Lab., Golden CO.
-
(1995)
Dynamic Stall Occurrence on a Horizontal Axis Wind Turbine Blade.
-
-
Shipley, D.1
Miller, M.2
Robinson, M.3
-
7
-
-
84896832841
-
-
AIAA 95-0526. 33rd Aerospace Sciences Meeting and Exhibit
-
Robinson, M., Galbraith R, Shipley, D., and Miller, M., 1995. “Unsteady Aerodynamics of Wind Turbines.” AIAA 95-0526. 33rd Aerospace Sciences Meeting and Exhibit.
-
(1995)
Unsteady Aerodynamics of Wind Turbines.
-
-
Robinson Galbraith, M.1
Shipley, R.D.2
Miller, M.3
-
8
-
-
0029836568
-
Unsteady aerodynamics associated with a horizontal axis wind turbine
-
Huyer, S., Simms, D., and Robinson, M., 1996. “Unsteady Aerodynamics Associated with a Horizontal Axis Wind Turbine.” ALAA J., 34. No. 7. pp. 1410-1419.
-
(1996)
ALAA J.
, vol.34
, Issue.7
, pp. 1410-1419
-
-
Huyer, S.1
Simms, D.2
Robinson, M.3
-
9
-
-
0025513240
-
Yaw loads and motions of a horizontal axis wmd turbine
-
Hansen, A., Butterfield, C., and Cui, X., 1990. “Yaw Loads and Motions of a Horizontal Axis Wmd Turbine.” J. Sol. Energy Eng. 112. No. 4, pp. 310-314.
-
(1990)
J. Sol. Energy Eng.
, vol.112
, Issue.4
, pp. 310-314
-
-
Hansen, A.1
Butterfield, C.2
Cui, X.3
-
10
-
-
0024091434
-
Three-dimensional \brtex systems of finite wings
-
Freymuth, P., 1988, “Three-Dimensional \brtex Systems of Finite Wings.” J. of Aircraft. 25. No. 10. pp. 971-972.
-
(1988)
J. Of Aircraft
, vol.25
, Issue.10
, pp. 971-972
-
-
Freymuth, P.1
-
11
-
-
0346066152
-
Unsteady surface pressure measurements on a pitching wing
-
26th Aerospace Sciences Meeting
-
Robinson M. and Wissler, J., 1988, “Unsteady Surface Pressure Measurements on a Pitching Wing.” AIAA SS-032S. ALAA. 26th Aerospace Sciences Meeting.
-
(1988)
AIAA SS-032S. ALAA
-
-
Robinson, M.1
Wissler, J.2
-
12
-
-
0008883251
-
-
UTRC Report R92-95S325-6
-
Lorber, P., Carta, F., and Covino, A., 1992. “An Oscillating Three- Dimensional Wing Experiment: Compressibility. Sweep. Rate. Waveform, and Geometry Effects on Unsteady Separation and Dynamic Stall.” UTRC Report R92-95S325-6.
-
(1992)
An Oscillating Three- Dimensional Wing Experiment: Compressibility. Sweep. Rate. Waveform, and Geometry Effects on Unsteady Separation and Dynamic Stall.
-
-
Lorber, P.1
Carta, F.2
Covino, A.3
-
13
-
-
4244014821
-
Flow field structure and development near the root of a straight wing pitching at constant rate
-
22nd Fluid Dynamics- Plasma Dynamics and Lasers Conf
-
Schreck, S., Addington G., and Luttges, M., 1991, “Flow Field Structure and Development Near the Root of a Straight Wing Pitching at Constant Rate.” ALAA 91-1793, AIAA 22nd Fluid Dynamics- Plasma Dynamics and Lasers Conf.
-
(1991)
ALAA 91-1793, AIAA
-
-
Schreck, S.1
Addington, G.2
Luttges, M.3
-
14
-
-
0028464109
-
Unsteady vortex dynamics and surface pressure topoloaes on a finite pitching wing
-
Schreck, S., and Helm, H., 1994, “Unsteady Vortex Dynamics and Surface Pressure Topoloaes on a Finite Pitching Wing.”J. Aircr., 31, No. 4. pp. 899- 907.
-
(1994)
J. Aircr.
, Issue.4
-
-
Schreck, S.1
Helm, H.2
-
15
-
-
27744570513
-
2-d and 3-d oscillating wing aerodynamics for a ranee of angles of attack including stall
-
Piziali, R. 1994. “2-D and 3-D Oscillating Wing Aerodynamics for a Ranee of Angles of Attack Including StalL” NASA TM 4632.
-
(1994)
NASA TM
, pp. 4632
-
-
Piziali, R.1
-
16
-
-
84895752998
-
-
Paper No. 2-3, 21st European Rotorcraft Forum
-
Galbraith, R., Co ton, F., Jiang, D., and Gilmour, R. 1995, “Preliminary Results from a Three-Dimensional Dynamic Stall Experiment of a Finite Wing.” Paper No. 2-3, 21st European Rotorcraft Forum.
-
(1995)
Preliminary Results from a Three-Dimensional Dynamic Stall Experiment of a Finite Wing.
-
-
Galbraith Co Ton, R.F.1
Jiang, D.2
Gilmour, R.3
-
17
-
-
0032654597
-
An experimental study- of dynamic stall on a finite wing
-
Coton, F., and Galbraith R. 1999. “An Experimental Study- of Dynamic Stall on a Finite Wing.” Aeronaut, J., 103. No. 1023, pp. 229-236.
-
(1999)
Aeronaut, J.
, vol.103
, Issue.1023
, pp. 229-236
-
-
Coton, F.1
Galbraith, R.2
-
18
-
-
0347901649
-
Hawt dynamic stall response asymmetries under yawed flow conditions
-
38th Aerospace Sciences Meeting and Exhibit
-
Schreck, S., Robinson, M., Hand M., and Sunms, D., 2000. “HAWT Dynamic Stall Response Asymmetries Under Yawed Flow Conditions,” AIAA 2000-0040, 38th Aerospace Sciences Meeting and Exhibit.
-
(2000)
AIAA 2000-0040
-
-
Schreck, S.1
Robinson, M.2
Hand, M.3
Sunms, D.4
-
19
-
-
0347234682
-
-
(“Profile Investigations on a Rotating Airscrew”), Dissertation. Got-tmgen; Mitt. Max-Planck-Institut fur Stromungsforschung Gottingen Nr. 2
-
Himmelskamp, H., 1945, “Profiluntersuchungen an einem umhufenden Propeller” (“Profile Investigations on a Rotating Airscrew”), Dissertation. Got-tmgen; Mitt. Max-Planck-Institut fur Stromungsforschung Gottingen Nr. 2.
-
(1945)
Profiluntersuchungen an Einem Umhufenden Propeller
-
-
Himmelskamp, H.1
-
20
-
-
85003212475
-
Delaying effect of rotation on laminar separation
-
Bank, W., and Gadd, G., 1963. “Delaying Effect of Rotation on Laminar Separation.” AIAA J, 1, No. 4, pp. 941-942.
-
(1963)
AIAA J
, vol.1
, Issue.4
, pp. 941-942
-
-
Bank, W.1
Gadd, G.2
-
21
-
-
85007715093
-
Laminar boundary layers on helicopter rotor: In forward flight
-
McCroskey, W., and Yaggy, P., 1968. “Laminar Boundary Layers on Helicopter Rotor: in Forward Flight.” AIAA J., 6. No. 10, pp. 1919-1926.
-
(1968)
AIAA J.
, vol.6
, Issue.10
, pp. 1919-1926
-
-
McCroskey, W.1
Yaggy, P.2
-
23
-
-
0025019195
-
On the relative importance of rotational unsteady and three-dimensional effects on the hawt rotor aerodynamics
-
Madsen, H., and Christensen, H., 1990. “On the Relative Importance of Rotational Unsteady and Three-Dimensional Effects on the HAWT Rotor Aerodynamics.” Wind Eng. 14. No. 6. pp. 405-415.
-
(1990)
Wind Eng
, vol.14
, Issue.6
, pp. 405-415
-
-
Madsen, H.1
Christensen, H.2
-
24
-
-
0026868448
-
Wind tunnel investigation of stall aerodynamics for a 1.0 m horizontal axis rotor
-
Barnsley, M., and Welhcome, J., 1992. “Wind Tunnel Investigation of Stall Aerodynamics for a 1.0 m Horizontal Axis Rotor.” J. Wind. Ens. Ind Aero- dyn., 39, pp. 11-21.
-
(1992)
J. Wind. Ens. Ind Aero- Dyn.
, vol.39
, pp. 11-21
-
-
Barnsley, M.1
Welhcome, J.2
-
25
-
-
0026798935
-
Static pressure measurements on a rotatmg and a non- rotating 2.375 m wind turbine blade. Comparison with 2d calculations
-
Ronsten, G., 1992, “Static Pressure Measurements on a Rotatmg and a Non- Rotating 2.375 m Wind Turbine Blade. Comparison with 2D Calculations.” J. Wind. Eng. Ind. Aerodyn. 39. pp. 105-11S.
-
(1992)
J. Wind. Eng. Ind. Aerodyn.
, vol.39
, pp. 105-118
-
-
Ronsten, G.1
-
26
-
-
0041727547
-
-
NREL TP-257-4655, National Renewable Energy Lab., Golden. CO
-
Butterfield C., Musial, W., and Simms, D., 1992, “Combined Experiment Phase I Final Report.” NREL TP-257-4655, National Renewable Energy Lab., Golden. CO.
-
(1992)
Combined Experiment Phase I Final Report.
-
-
Butterfield, C.1
Musial, W.2
Simms, D.3
-
27
-
-
0347901646
-
-
NRELTP- 442-6916. National Renewable Energy Laboratory, Golden. CO
-
Miller, M., Shipley, D., Young, T., Robinson, M., Luttges, M., and Simms, D., 1995, “Combined Experiment Phase II Data Characterization.” NRELTP- 442-6916. National Renewable Energy Laboratory, Golden. CO.
-
(1995)
Combined Experiment Phase II Data Characterization.
-
-
Miller, M.1
Shipley, D.2
Young, T.3
Robinson, M.4
Luttges, M.5
Simms, D.6
-
28
-
-
0029230233
-
An overview of the unsteady aerodynamics experiment phase iii data acquisition system and instrumentation
-
Houston. TX
-
Fingersh, L., Simms, D., Butterfield, C., and Jenks, M., 1995, “An Overview of the Unsteady Aerodynamics Experiment Phase III Data Acquisition System and Instrumentation.” ASME Energy and Environment Expo ‘95. Houston. TX.
-
(1995)
ASME Energy and Environment Expo ‘95.
-
-
Fingersh, L.1
Simms, D.2
Butterfield, C.3
Jenks, M.4
-
29
-
-
0142127918
-
-
NREL’TP-500-25950. National Renewable Enersv Lab., Golden. CO
-
Simms, D., Hand M., Fmgersh, L., and Jager, D., 1999, “Unsteady Aerodynamics Experiment Phase II-IV Test Configurations and Available Data Campaigns.” NREL’TP-500-25950. National Renewable Enersv Lab., Golden. CO.
-
(1999)
Unsteady Aerodynamics Experiment Phase II-IV Test Configurations and Available Data Campaigns.
-
-
Simms, D.1
Hand, M.2
Fmgersh, L.3
Jager, D.4
-
30
-
-
0346641430
-
-
NREL’ TP-500-27599. National Renewable Energy Lab., Golden. CO
-
Simms, D., Schreck, S., Hand, M., Fmgersh, L., Cotrell, J., Pierce, K., and Robinson, M., 1999. “Plans for Testing the NREL Unsteady Aerodynamics Experiment 10-m Diameter HAWT m the NASA Ames Wmd Tunnel.” NREL’ TP-500-27599. National Renewable Energy Lab., Golden. CO.
-
(1999)
Plans for Testing the NREL Unsteady Aerodynamics Experiment 10-M Diameter HAWT M the NASA Ames Wmd Tunnel.
-
-
Simms, D.1
Schreck, S.2
Hand, M.3
Fmgersh, L.4
Cotrell, J.5
Pierce, K.6
Robinson, M.7
-
31
-
-
0347901647
-
-
NREL’SR 500-26173 National Renewable Eneigy Lab., Golden, CO
-
Giguere, P., and Selig, M., 1999. “Design of a Tapered and Twisted Blade for the NREL Combined Experiment Rotor.” NREL’SR 500-26173 National Renewable Eneigy Lab., Golden, CO.
-
(1999)
Design of a Tapered and Twisted Blade for the NREL Combined Experiment Rotor.
-
-
Giguere, P.1
Selig, M.2
-
32
-
-
0142127918
-
-
NREL’TP-500-25950. National Renewable Energy Lab., Golden. CO
-
Simms, D., Hand M., Fmgersh, L., and Jager, D., 1999. “Unsteady Aerodynamics Experiment Phases II-IV Test Configuration and Available Data Campaigns.” NREL’TP-500-25950. National Renewable Energy Lab., Golden. CO.
-
(1999)
Unsteady Aerodynamics Experiment Phases II-IV Test Configuration and Available Data Campaigns.
-
-
Simms, D.1
Hand, M.2
Fmgersh, L.3
Jager, D.4
-
33
-
-
0003807318
-
-
NRELTP-442-7393, National Renewable Energy Lab., Golden CO
-
Shipley, D., Miller, M., Robinson, M., Luttges, M., and Simms, D., 1995, “Techniques for the Determination of Local Dynamic Pressure and Angle of Attack on a Horizontal Axis Wmd Turbine.” NRELTP-442-7393, National Renewable Energy Lab., Golden CO.
-
(1995)
Techniques for the Determination of Local Dynamic Pressure and Angle of Attack on a Horizontal Axis Wmd Turbine.
-
-
Shipley, D.1
Miller, M.2
Robinson, M.3
Luttges, M.4
Simms, D.5
-
35
-
-
84998785465
-
An experimental investiganon of an aufoil undergoing large amplitude pitching motions
-
23rd Aerospace Sciences Meeting
-
Walker, J., Helm, H., and Strickland, J., 1985. “An Experimental Investiganon of an Aufoil Undergoing Large Amplitude Pitching Motions.” AIAA 85-0039. AIAA 23rd Aerospace Sciences Meeting.
-
(1985)
AIAA 85-0039. AIAA
-
-
Walker, J.1
Helm, H.2
Strickland, J.3
-
37
-
-
0344390129
-
Measurements of the dynamic stall vortex convection speed
-
Green, R., Galbraith, R. and Niven A., 1992, “Measurements of the Dynamic Stall Vortex Convection Speed” Aeronaut, J., pp. 319-325.
-
(1992)
Aeronaut, J.
, pp. 319-325
-
-
Green, R.1
Galbraith, R.2
Niven, A.3
-
38
-
-
0347327482
-
-
NRELTP-442-7S17, National Renewable Energy Lab., Golden. CO
-
Reuss Ramsay, R., Hoffman, M., and Gregorek, G., 1995, “Effects of Gnt Roughness and Pitch Oscillations on the 8809 AirfoiL” NRELTP-442-7S17, National Renewable Energy Lab., Golden. CO.
-
(1995)
Effects of Gnt Roughness and Pitch Oscillations on the 8809 Airfoil
-
-
Reuss Ramsay Hoffman, R.M.1
Gregorek, G.2
-
39
-
-
85088205284
-
Chordwise propagation of dynamic stall cells on an oscillating airfoil
-
13th Aerospace Sciences Meeting
-
Carta, F., 1975, “Chordwise Propagation of Dynamic Stall Cells on an Oscillating AirfoiL” AIAA 75-25. AIAA 13th Aerospace Sciences Meeting.
-
(1975)
AIAA 75-25. AIAA
-
-
Carta, F.1
-
40
-
-
84894450080
-
Unsteady separated flow structure: Extended k range and oscillations through zero pitch angle
-
26th Aerospace Sciences Meeting
-
Schreck, S., and Luttges, M., 1988. “Unsteady Separated Flow Structure: Extended K Range and Oscillations Through Zero Pitch Angle.” AIAA SS-0325, AIAA 26th Aerospace Sciences Meeting.
-
(1988)
AIAA SS-0325, AIAA
-
-
Schreck, S.1
Luttges, M.2
-
42
-
-
84963568189
-
Encoding of three-dimensional unsteady separated flow field dynamics in neural network architectures
-
33rd Aerospace Sciences Meeting and Exhibit
-
Schreck, S., and Faller, W., 1995. “Encoding of Three-Dimensional Unsteady Separated Flow Field Dynamics in Neural Network Architectures.” AIAA 95-0103. AIAA 33rd Aerospace Sciences Meeting and Exhibit.
-
(1995)
AIAA 95-0103. AIAA
-
-
Schreck, S.1
Faller, W.2
-
43
-
-
0346696952
-
Experimental investigation of the mechanisms underlying vortex kinematics m unsteady separated flows
-
Boulder. CO
-
Schreck, S., 1989, “Experimental Investigation of the Mechanisms Underlying Vortex Kinematics m Unsteady Separated Flows.” (Dissertation) Graduate School. Univ. of Colorado. Boulder. CO.
-
(1989)
(Dissertation) Graduate School. Univ. Of Colorado
-
-
Schreck, S.1
-
44
-
-
85003441532
-
Controlled three-dimensionality in unsteady separated flow about a sinusoidally oscillating flat plate
-
28th Aerospace Sciences Meeting January’
-
Homer, M., Addington, G., Young, J., and Luttges, M., 1990, “Controlled Three-Dimensionality in Unsteady Separated Flow About a Sinusoidally Oscillating Flat Plate.” AIAA 90-06S9. 28th Aerospace Sciences Meeting January’.
-
(1990)
AIAA 90-06S9
-
-
Homer, M.1
Addington, G.2
Young, J.3
Luttges, M.4
-
45
-
-
0019045385
-
Flowfield model for a rectangular planform wing beyond stall
-
Winkelmann, A., and Barlow, J., 1980, “Flowfield Model for a Rectangular Planform Wing Beyond StalL” AIAA J., 13. No, 8. pp. 1006-1007.
-
(1980)
AIAA J.
, vol.13
, Issue.8
, pp. 1006-1007
-
-
Winkelmann, A.1
Barlow, J.2
|