-
3
-
-
0346953365
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"The Present Basis of Axial Flow Compressor Design: Part I - Cascade Theory and Performance"
-
Aeronautical Research Council R. and M. No. 2095
-
Howell, A. R., 1942, "The Present Basis of Axial Flow Compressor Design: Part I-Cascade Theory and Performance," Aeronautical Research Council R. and M. No. 2095.
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Howell, A.R.1
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4
-
-
0003416203
-
"A Theoretical Investigation of the Effect of Profile Shape on the Performance of Aerofoils in Cascade"
-
Aeronautical Research Council R. and M. No. 2384
-
Carter, A. D. S., and Hughes, H. P., 1950, "A Theoretical Investigation of the Effect of Profile Shape on the Performance of Aerofoils in Cascade," Aeronautical Research Council R. and M. No. 2384.
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Carter, A.D.S.1
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5
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0001722651
-
"Loss and Stall Analysis of Compressor Cascades"
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Lieblein, S., 1959, "Loss and Stall Analysis of Compressor Cascades," ASME J. Basic Eng., 81, p. 3.
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ASME J. Basic Eng.
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-
-
Lieblein, S.1
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6
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0013417496
-
"The Early History of the Whittle Jet Propulsion Gas Turbine"
-
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Whittle, F.1
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7
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0347496725
-
"An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines"
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Aeronautical Research Council R. and M. 2891
-
Ainley, D. G., and Mathieson, G. C. R., 1955, "An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines," Aeronautical Research Council R. and M. 2891.
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Ainley, D.G.1
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9
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0346953358
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"A Theory of the Direct and Inverse Problems of Compressible Flow Past Cascade of Arbitrary Aerofoils"
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Wu, Chung-hua, and Brown, C. A., 1952, "A Theory of the Direct and Inverse Problems of Compressible Flow Past Cascade of Arbitrary Aerofoils," J. Aeronaut. Sci., pp. 183-196.
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Wu, C.-h.1
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10
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0347064919
-
"Design of Two-dimensional Channels With Prescribed Velocity Distributions Along the Channel Walls"
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NACA Tech. Notes 2593
-
Stanitz, J. D., 1952, "Design of Two-dimensional Channels With Prescribed Velocity Distributions Along the Channel Walls," NACA Tech. Notes 2593, 2595.
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-
-
Stanitz, J.D.1
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11
-
-
16244392536
-
"Approximate Design Method for High-Solidity Blade Elements in Compressors and Turbines"
-
NACA Tech. Note 2408
-
Stanitz, J. D., 1951, "Approximate Design Method for High-Solidity Blade Elements in Compressors and Turbines," NACA Tech. Note 2408.
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-
Stanitz, J.D.1
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13
-
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34250586577
-
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Kraft, H., 1958, "Development of a Laminar Wing Type Turbine Bucket," ZAMP, 404.
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14
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16244384781
-
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NACA Report 778
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Garrick, J. E., 1944, "On the Plane Potential Flow Past a Lattice of Arbitrary Aerofoils," NACA Report 778.
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Garrick, J.E.1
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16
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0346323442
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Martensen, E.1
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17
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0346953364
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"Potential Flow Through Cascades-Extension to an Exact Theory"
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Aeronautical Research Council, CP 808
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Gostelow, J. P., 1962, "Potential Flow Through Cascades-Extension to an Exact Theory," Aeronautical Research Council, CP 808.
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Gostelow, J.P.1
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18
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Hobson, D.E.1
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19
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1-16
-
Stratford, B. S., 1959, "The Prediction of Separation of the Turbulent Boundary Layer. An Experimental Flow With Zero Skin Friction Throughout Its Region of Pressure Rise," J. Fluid Mech., pp. 1-16,17-35.
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Stratford, B.S.1
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21
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"Secondary Circulation in Fluid Flow"
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Ser. A
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22
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"Rotational Flow Through Cascades, Part I - The Components of Vorticity"
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Hawthorne, W. R., 1955, "Rotational Flow Through Cascades, Part I-The Components of Vorticity," Q. J. Mech. Appl. Math., 8, p. 266.
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23
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85135756656
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"Secondary Flow in Axial Flow Turbomachinery"
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Smith, L. H., 1953, "Secondary Flow in Axial Flow Turbomachinery," Trans. ASME, 77, p. 1065.
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-
Smith, L.H.1
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24
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0017440228
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"Three-Dimensional Flow Within a Turbine Passage"
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Langston, L. S., Nice, M. L., and Hooper, R. M., 1977, "Three-Dimensional Flow Within a Turbine Passage," ASME J. Eng. Gas Turbines Power, 99, pp. 21-28.
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Langston, L.S.1
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25
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0014814618
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"Improvements to the Ainley-Mathieson Method of Turbine Performance Prediction"
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Dunham, J., and Came, P. M., 1970, "Improvements to the Ainley-Mathieson Method of Turbine Performance Prediction," ASME J. Eng. Gas Turbines Power, A92, p. 252.
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-
Dunham, J.1
Came, P.M.2
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26
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0021412368
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-
Hah, C. A., 1984, "Navier-Stokes Analysis of Three-Dimensional Turbulent Flows Inside Turbine Blade Rows at Design and Off-Design Conditions," ASME J. Eng. Gas Turbines Power, 106, pp. 421-429.
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-
Hah, C.A.1
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29
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0345984643
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"A Computer Program for the Through Flow Fluid Mechanics in an Arbitrary Turbomachine Using a Matrix Method"
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Aeronautical Research Council R. and M. No. 3509
-
Marsh, H., 1968, "A Computer Program for the Through Flow Fluid Mechanics in an Arbitrary Turbomachine Using a Matrix Method," Aeronautical Research Council R. and M. No. 3509.
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30
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-
0003398823
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-
NACA Tech. Note 2604
-
Wu, Chung-Hua, 1952, "A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachine in Radial, Axial and Mixed Flow Types," NACA Tech. Note 2604.
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31
-
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0003832136
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"Tip Clearance Flows in Axial Compressors and Pumps"
-
California Institute of Technology, Hydrodynamics and Mechanical Engineering Laboratories, Report No. 5
-
Rains, D. A., 1954, "Tip Clearance Flows in Axial Compressors and Pumps," California Institute of Technology, Hydrodynamics and Mechanical Engineering Laboratories, Report No. 5.
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Rains, D.A.1
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32
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0347584436
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"Secondary Flow in Axial Compressors"
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Sc.D thesis, Gas Turbine Laboratory, M.I.T., Cambridge, MA
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Dean, R. C., 1954, "Secondary Flow in Axial Compressors," Sc.D thesis, Gas Turbine Laboratory, M.I.T., Cambridge, MA.
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Dean, R.C.1
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33
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0004520163
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"Leakage and Secondary Flow in Compressor Cascades"
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Aeronautical Research Council, R. and M. 3483
-
Lakshminarayana, B., and Horlock, J. H., 1967, "Leakage and Secondary Flow in Compressor Cascades," Aeronautical Research Council, R. and M. 3483.
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34
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0014844259
-
"Predicting the Tip Clearance Flow in Axial Flow Turbomachines"
-
Lakshminarayana, B., 1970, "Predicting the Tip Clearance Flow in Axial Flow Turbomachines," ASME J. Basic Eng., 92, pp. 467-482.
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-
Lakshminarayana, B.1
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35
-
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16244386984
-
"Performance of Cascades of Aerofoils, Royal Aircraft Establishment"
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36
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-
Taylor, E. S., 1957, "Problem of the Convergent Nozzle," Technical Note (unpublished) Gas Turbine Laboratory, M.I.T., Cambridge, MA.
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0003780030
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Krieger Publishing Company, Melbourne, FL
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Horlock, J.H.1
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38
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Horlock, J. H., and Marsh, H., 1971, "Flow Models for Turbomachinery," J. Mech. Eng. Sci., 13, pp. 358-368.
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39
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33745238270
-
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NASA TND 4525
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Katsanis T., 1968, "Computer Program for Calculating Velocities and Streamlines on a Blade-to-Blade Stream Surface of a Turbomachine," NASA TND 4525.
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Katsanis, T.1
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40
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85042205459
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"Calculation of Blade-to-Blade Flow in a Turbomachine by Streamline Curvature"
-
Aeronautical Research Council, R. and M. 3704
-
Wilkinson, D. H., 1972, "Calculation of Blade-to-Blade Flow in a Turbomachine by Streamline Curvature," Aeronautical Research Council, R. and M. 3704.
-
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-
-
Wilkinson, D.H.1
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41
-
-
85040279253
-
"A Mixed-Flow Cascade Passage Design Procedure Based on a Power Series Expansion"
-
ASME Paper 82-GT-121
-
Novak, R. A., and Haymann-Haber, G., 1982, "A Mixed-Flow Cascade Passage Design Procedure Based on a Power Series Expansion," ASME Paper 82-GT-121.
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42
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0036648908
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Smith, L. H., 2002, "Axial Compressor Aerodesign Evolution at General Electric," ASME J. Turbomach., 124, pp. 321-330.
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Smith, L.H.1
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43
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16244386331
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"Deviation Estimation for Axial-Flow Compressors Using Inviscid Flow Solutions"
-
ASME Paper 74-GT-74
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Miller, M. J., and Serovy, G. K., 1974, "Deviation Estimation for Axial-Flow Compressors Using Inviscid Flow Solutions," ASME Paper 74-GT-74.
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Miller, M.J.1
Serovy, G.K.2
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44
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-
0020782810
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45
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"The Calculation of Threedimensional Viscous Flow Through Multistage Turbomachines"
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46
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0000056578
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"Fluid Dynamics of Axial Compressors"
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War Emergency Issue
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48
-
-
0141666700
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"Predictions of the Flow in Repeating Stages of Axial Compressors Using Navier-Stokes Solvers"
-
ASME Paper 95-GT-199
-
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Bolger, J.J.1
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49
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-
0028525732
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Howard, M. A., Ivey, P. C., Barton, J. P., and Young, K. F., 1994, "End Wall Effects at Two Tip Clearances in a Multi-Stage Axial Flow Compressor With Controlled Diffusion Blading," ASME J. Turbomach., 106, pp. 635-647.
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"The Determination of End-Wall Blockage in Axial Flow Compressors - A Comparison Between Various Approaches"
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Horlock, J.H.1
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51
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0348214120
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"Secondary Loss Generation in a Linear Cascade of High-Turning Turbine Blades"
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ASME Paper 89-GT-47
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Harrison, S.1
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52
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0141802150
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