Selected GTL Reports

(We don't have copies of every report any more but if you're interested in one of these, send an email to Robin Courchesne-Sato and she'll see what she can do.)

Allmaras, S.R., "A Coupled Euler/Navier-Stokes Algorithm for 2-D Unsteady Transonic Shock/Boundary-Layer Interaction", 1989, 196.

Bartlett Jr., F., Greitzer, E.M., "Stalled Flow Performance of a Single Stage Transonic Compressor", 1978, 144.

Bates, S.C., "Luminescent Visualization of Molecular and Turbulent Transport in a Plane Shear Layer", 1977, 134.

Beasley, C.O., Meier, H.K., van Rij, W.I., McCune, J.E., "Calculation of a Self-Consistent, Low Frequency Electrostatic Field in the Drift-Kinetic Approximation", 1977, 135.

Buliava, G.P., Crawley, E.F., "Design and Evaluation of a Pulsing Jet Injector for Rotating Fan Excitation", 1985, 185.

Bush, R.H., "Time Accurate Internal Flow Solutions of the Thin Shear Layer Equations", 1981, 156.

Bush, R.H., "Prediction of Complex, Viscous, Compressible, Internal Flow Using Implicit Finite Difference Methods", 1983, 175.

Capece, V.R., "Investigation of Turbocharger Stall: I–Facility Design and Construction and Initial Performance Data", 1982, 165.

Chen, L.T., "ThermaL Stress and Gas Bending Effects in Vibrations of Compressor Rotor Stages", 1977, 139.

Chen, L.T., McCune, J.E., "Comparison of Three-Dimensional Quasi-Linear Large Swirl Theory with Measured Outflow From a High-Work Compressor Rotor", 1975, 128.

Cheng, P., "Effects of Compressor Hub Treatment on Stator Stall and Presssure Rise", 1982, 167.

Cheng, W.K., "Uniform-Inlet Three-Dimensional Transonic Beltrami Flow Through a Ducted Fan", 1977, 130.

Cheng, W.K., "Turbulent Mixing in Swirling Flow", 1978, 143.

Cho, Y-C, Ingard, K.U., "Attenuation of Sound in Lined Circular Ducts", 1974, 119.

Cho, Y-C, Ingard, K.U., Addendum to 119 "Attenuation of Sound in Lined Circular Ducts", 1975, 120.

Ciacci, F., "Theoretical Investigation of Volute Effect on Low-Flow Dynamic Stability in a Centrifugal Pump", 1992, 214.

Crawley, E.F., "Measurements of Aerodynamic Damping in the MIT Transonic Rotor", 1981, 157.

Crook, A.J., "Numerial Investigation of Endwall/Casing Treatment Flow Phenomena", 1989, 200.

Cumpsty, N.A., "Aerodynamics of Aircraft Engines–Stride and Stumbles", 1992, 213.

Cumpsty, N.A., Greitzer, E.M., "A Simple Model for Compressor Stall Cell Propagation", 1980, 148.

Dang, T.Q., McCune, J.E., "A Two-Dimensional Design Method for Highly-Loaded Blades in Turbomachines", 1983, 173.

Dawson, D.B., "Condensation of Supersaturated Organic Vapors in a Supersonic Nozzle", 1967, 90.

Dean, R.C. Jr., "The Influence of Tip Clearance on Boundary-Layer Flow in a Rectilinear Cascade", 1954, 27-3.

De Siervi, F., "A Flow Visualization Study of the Inlet Vortex Phenomenon", 1981, 159.

Denzi, S., "Effects of Inlet Conditions on Centrifugal Diffuser Performance", 1997, 225.

Drela, M. "Two-Dimensional Transonic Aerodynamic Design and Analysis Using the Euler Equations", 1986, 187.

Drela, M., Thompkins, W.T. Jr., "A New Transformation and Integration Scheme for the Compressible Boundary Layer Equations, and Solutions Behavior at Separation", 1983, 172.

Drum, N.J., "Investigation of the Flow in an Axial-to-Radial Diffuser", 1971, 109.

Ducharme, E.H., Crawley, E.F., "Velocity Scaled Aeroelastic Testing of an Unducted Fan", 1987, 191.

Ducharme, E.H., Mokadam, D.R., Crawley, E.F., "Forced Rotating Whirl Tests on a Cantilevered Turbonfan", 1985, 182.

Duff, K.M., "Condensation of Carbon Dioxide in Supersonic Nozzles", 1964, 76.

Duff, K.M., "Non-equiliibrium Condensation of Carbon Dioxide in Supersonic Nozzles", 1966, 84.

Dugundji, J., "Flutter Analysis of a Tuned Rotor with Rigid and Flexible Disks", 1979, 146.

Dugundji, J., Buellesback, M.M., Wright, M.A., "Some Observations of the Vibrations of Slender Rotating Shafts", 1982, 163.

Dugundji, J., Bundas, D.J,, "Flutter and Forced Response of Mistuned Rotors Using Standing Wave Analysis", 1983, 170.

Durali, M., "Rotor Wake Behavior in a Transonic Compressor Stage and Its Effect on the Loading and Performance of the Stator", 1980, 149.

Eastland, A.H J., "Investigation of Compressor Performance in Rotating Stall: I–Facility Design and Construction and Initial Steady State Measurements", 1982, 164.

Epstein, A.H., "Fluorescent Gaseous Tracers for Three-Dimensional Flow Visualization", 1974, 117.

Epstein, A.H., "Fluorescent Visualization for Turbomachine Research", 1978, 142.

Epstein, A.H., "Quantitative Density Visualization in a Transonic Compressor Rotor", 1975, 124.

Epstein, A.H., Guenette, G.R., Norton, R.J.G, "The Design of the MIT Blowdown Turbine Facility", 1985, 183.

Epstein, A.H., Kerrebrock, J.L., Koo, J.J., Preiser, U.Z., "Rotational Effects on Impingement Cooling", 1985, 184.

Felici, H.M., "A Coupled Eulerian/Lanrangian Meghod for the Solution of Three-Dimensional Vortical Flows", 1992, 211.

Fernolz, H., Gibson, P., "Experiments on Turbulent Boundary Layers Along a Circular Cylinder With and Without Separation", 1967, 91.

Figueiredo, W.R., "Spherical Pressure Probe for Retrieving Freestream Pressure and Directional Data", 1977, 137.

Filipenco, V.G., "Experimental Investigation of Flow Distortion Effects on the Performance of Radial Discrete-Passage Diffusers", 1991, 206.

Fink, D.A., "Surge Dynamics and Unsteady Flow Phenomena in Centrifugal Compressors", 1988, 193.

Fritsch, G., "An Analytical and Numerical Study of the Second-Order Effects of Unsteadiness on the Performance of Turbomachines", 1992, 210.

Gardow, E.B., "The Three-Dimensional Turbulent Boundary Layer in a Free Vortex Diffuser", 1958, 42.

Garnier, V.H., "Experimental Investigation of Rotating Waves as a Rotating Stall Inception Indication in Compressors", 1989, 198.

Gertz, J., "Unsteady Design-Point Flow Phenomena in Transonic Compressors", 1986, 188.

Giles, M., "UNSFLO: A Numerical Method for the Calculation of Unsteady Flow in Turbomachinery", 1991, 205.

Giles, M.B., "Newton Solution of Steady Two-Dimensional Transonic Flow", 1985, 186.

Giles, M.B., "UNSFLO: A Numerical Method for Unsteady Inviscid Flow in Turbomachinery", 1988, 195.

Giles, M.B., Thompkins, W.T. Jr., "Asymptotic Analysis of Numerical Wave Propagation in Finite Difference Equations", 1983, 171.

Goldberg, P., "Upstream History and Apparent Stress in Turbulent Boundary Layers", 1966, 85.

Gong, Y., "A Computational Model for Rotating Stall and Inlet Distortions in Multistage Compressors," 1999, 230.

Gopalakrishnan, S., "An Unconventional Blade Design for Axial Compressors", 1969, 98.

Graf, M.B., Wong, T.S., Greitzer, E.M., Marble, F.E., Tan, C.S., Shin, H-W., Wisler, D.C., "Effects of Non-Axisymmetric Tip Clearance on Axial Compressor Performance and Stability", 1997, 228.

Gysling, D.L., "Dynamic Control of Rotating Stall in Axial Flow Compressors Using Aeromechanical Feedback", 1993 219.

Hall, K.C, "A Linearized Euler Analysis of Unsteady Flows in Turbomachinery", 1987, 190.

Hall, K.C., Crawley, E.F., "Optimal Mistuning for Enchanced Aeroelastic Stability of Transonic Fans", 1983, 176.

Handa, H., "The Development of a Perturbed, Incompressible, Turblent Boundary Layer", 1969, 96.

Hawthorne, W.R., "On the Theory of Shear Flow", 1966, 88.

Hawthorne, W.R., "On the Theory of Shear Flow" (supplement and corrigenda to #88), 1967, 93.

Haymann-Haber, G., "Computational Study of the Flow in a Transonic Axial Compressor Using an Inviscid, Three-Dimensional Finite Difference Method", 1979, 145.

Haynes, J. M., "Active Control of Rotating Stall in a Three-Stage Axial Compressor", 1993, 218.

Hill, P.G., "Laminar Boundary Layers in Oscillatory Flow", 1958, 45.

Hill, P.G., "Turbulent Wakes in Pressure Gradients", 1962, 65.

Hill, P.G., "Homogenous Nucleation of Supersaturated Water Vapor in Nozzles", 1965, 78.

Hill, P.G. "Incompressible Jet Mixing in Converging-Diverging Axisymmetric Ducts", 1965, 83.

Hill, P.G., Moon, I.M., "Effects of Coriolis on the Turbulent Boundary Layer in Rotating Fluid Machines", 1962, 69.

Hinck, H., "Secondary Flow in a Compressor Cascade", 1959, 50.

Horlock, J.H., "A Rapid Calculation Method for the "Off-Design"Performance of Compressors and Turbines, 1957, 40.

Hoying, D.A., "Blade Passage Flow Structure Effects on Axial Compressor Rotating Stall Inception", 1996, 224.

back to top

 

Ingard, K.U., "Notes on Hydroacoustics", 1994, 220.

Isomura, K., "A Numerical Investigation of a Flutter in a Transonic Fan", 1996, 223.

Jaeger, H.L., "Condensation of Supersaturated Ammonia and Water Vapor in Supersonic Nozzles" 1966, 86.

Jansen, W., "Incompressible Fluid Flow in a Radial Vaneless Diffuser" 1959, 52.

Jansen, W., "Compressible Fluid Flow in a Radial Vaneless Diffuser", 1960, 58.

Jansen, W., "Quasi-unsteady Flow in a Radial Vaneless Diffuser", 1960, 60.

Johnston, J.M., "Stall Onset Observation of a Discrete Passage Diffuser", 1993, 217.

Johnston, J.P., "Experimental Data On Three-Dimensional Flow in a Centrifugal Compressor Diffuser", 1954, 27-7.

Johnston, J.P., "Three-Dimensional Turbulent Boundary Layer", 1957, 39.

Kerrebrock, J.L., "Small Disturbances in Compressor Annuli with Swirl, Throughflow and Entropy Variation", 1970, 104.

Kerrebrock, J.L., "The M.I.T. Blowdown Compressor Facility", 1972, 108.

Kerrebrock, J.L., "Small Disturbances in Turbomachine Annuli with Swirl", 1975, 125.

Khabbaz, G.R., "The Infulence of Tip Clearance on Stall Limits of a Rectilinear Cascade of Compressor Blades", 1959, 54.

Khalak, A., "Parametric Dependencies of Aeroengine Flutter for Flutter Clearance Applications", 2000, 231.

Kiang, D.T., Tam, C.K.W., Kerrebrock, J.L., "Noise Generation by Shock-Turbulence Interaction", 1970, 102.

Koo, J., "Channel Flow Modeling of Impingement Cooling of a Rotating Turbine Blade", 1984, 181.

Kotansky, D.R., "Thin Airfoils in Rotational Flow", 1965, 80.

Kotidis, P.A., "Unsteady Radial Transport in a Transonic Compressor Stage", 1989, 199.

Kreatsoulas, J.C., ‘Experimental Study of Impingement Cooling in Rotating Turbine Blades", 1983, 178.

Kremmer, M., Okurounmu, O., "Condensation of Ammonia Vapor During Rapid Expansion", 1965, 79.

Kriebel, A.R., "Stall Propagation in a Cascade of Airfoils, 1956, 36.

Kriebel, A.R., Stenning, A.H., "A Cascade Tunnel for Investigation of Rotating Stall", 1954, 27-1.

Kriebel, A.R., Schwind, R.G., Seidel, B., "Stall Propagation in a Cascade of Airfoils", 1956, 34.

Kubota, S., "Cascade Performance with Accelerated or Decelerated Axial Velocity", 1959, 56.

Kumar, A., Kerrebrock, J.L., "Rotor Wake Transport in Turbomachine Stators", 1971, 103.

Launder, B.E., "The Turbulent Boundary Layer in a Strongly Negative Pressure Gradient", 1963, 71.

Launder, B.E., "Laminarization of the Turbulent Boundary Layer by Acceleration", 1964, 77.

Lavrich, P.L., "Time Resolved Measurements of Rotating Stall in Axial Flow Compressors", 1988, 194.

Lazarus, K.B., Crawley, E.F., "Induced Strain of Actuation of Composite Plates", 1989, 197.

Lee, N.K.W, "Effects of Compressor Endwall Suction and Blowing on Stability Enhancement", 1988, 192.

Lefcort, M.D., "Wake Induced Unsteady Blade Forces in Turbo-Machines", 1962, 70.

Lindquist, D.R., "Computation of Unsteady Transonic Flowfields Using Shock Capturing and the Linear Perturbation Euler Equations", 1991, 207.

Liu, W., "Design and Analysis of an Experimental Facility for Inlet Vortex Investigation", 1982, 166.

Louis, J.F., Demirjian, A.M., Topping, R.F., "Heat Transfer Measurements in Turbines", 1972, 113.

Louis, J.F., Letty, R.M., Patel, J.R., "A Systematic Study of Supersonic Jet Noise", 1971, 106.

Martinez-Sanchez, M., Gauthier, R.P., "Blade Scale Effects of Tip Leakage", 1990, 202.

McCune, J.E., Dharwadkar, S.P., "Lifting-Line Theory for Subsonic Axial Compressor Rotors", 1972, 110.

McCune, J.E., "Three-Dimensional Inviscid Flow Through A Highly-Loaded Transonic Compressor Rotor", 1976, 126.

McGahan, W., "The Incompressible, Turbulent Wall Jet in a an Adverse Pressure Gradient", 1965, 82.

Mellor, G.L. Jr., "Theoretical Consideration of Secondary Flow", 1954, 27-2.

Mellor, G.L. Jr., " The Aerodynamic Performance of Axial Compressor Cascades with Application to Machine Design", 1957, 38.

Menis, M., "Effect of Vortex Decay on Pipe Flow", 1960, 61.

Meserole, J.S., "Detection Filters for Fault-Tolerant Control of Turbofan Engines", 1981, 158 (also Draper Lab Report T751).

Montgomery, S.R., "The Design of a Low Speed Cascade Tunnel", 1958, 43.

Montgomery, S.R., "Three-Dimensional Flow in Compressor Cascades", 1958, 48.

Montgomery, S.R. and Braun, J.J., "An Investigation of Rotating Stall in a Single Stage Axial Compressor", 1955, 29.

Moon, I.M., "Effects of Coriolis Force on the Turbulent Boundary Layer in Adverse Pressure Gradients", 1964, 74.

Moore, J., "Effects of Coriolis on Turbulent Flow in Rotation Rectangular Channels", 1967, 89.

Moore, J., "The Development of Turbulent Boundary Layers in Centrifugal Machines", 1969, 99.

Moore, R.W. Jr., Richardson, D.L., "Axisymmetric Solutions of the Flow Through a Single-Stage Axial Compressor", 1954, 27-5.

Moore, R.W. Jr., Richardson, D.L., "A Study of the End Wall Boundary Layer in an Axial Compressor Blade Row", 1955, 33.

Moore, R.W. Jr., Schneider, K.H., "Measurements of Flow Through a Single-Stage Axial Compressor", 1954, 27-6.

Moore, R.W. Jr., Nelson, W.G., Prasad, A., Richardson, D.L., Turner, J.R., "Experimental Techniques for Three-Dimensional Flow Research", 1954, 27-8.

Morton, H.L., "Effect of Swirl on Turbulent Jets in Ducted Streams", 1968, 95.

Moses, H.L., "Boundary Layer Separation", 1962, 68.

Moses, H.L, "The Behavior of Turbulent Boundary Layers in Adverse Pressure Gradients", 1964, 73.

Moses, H.L., Chappell, J.R., Goldberger, T., "Boundary Layer Separation in Internal Flow", 1965, 81.

Mullan, P.J., "An Investigation of Cavitating Inducers for Turbopumps", 1959, 53.

Nash-Webber, J.L., "Wall Shera-Stress and Laminarization in Accelerated Turbulent Compressible Boundary-Layers" 1968, 94.

Nelson, W.G., "Skewed Turbulent Boundary Layers", 1959, 55.

Ng, W.F., "Detailed Time Resolved Measurements and Analysis of Unsteady Flow in a Transonic Compressor", 1980, 150.

Ng, W.F., "Time-Resolved Stagnation Temperature Measurement in a Transonic Compressor Stage", 1983, 177.

Nice, G.R., Tseng, W-Y., Moses, H.L., "Separation of Turbulent, Incompressible Flow from a Curved, Backward-facing Step., 1966, 87.

back to top

 

Okurounmu, O., "Wave Drag in Transonic Axial Compressors", 1967, 92.

Oliver, D.A., "Time Dependent Magnetohydrodynamic Generator", 1974, 115.

Oliver, D.A., "The Prediction of Inter-Electrode Breakdown in Magnetohydrodynamic Generators" , 1974, 116.

Oliver, D.A., "Accurate, Efficient Difference Operators for the Turbulent Field Equations", 1975, 121.

Oliver, D.A., "Collapse of the Inter-Electrode Breakdown are in the Magnetic Field Direction", 1975, 122.

Oliver, D.A., Sparis, P., "Computational Studies of Three Dimensional Transonic Shear Flow: Work in Progress", 1970, 101.

Oliver, D.A., Byer, "Physical and Economic Models of Open Cycle Coal Burning MHD Power Generation System", 1972, 107.

Olsson, E.K.A, "Centrifugal Effect on the Boundary Layer on a Blade of an Axial Turbo-Machine", 1962, 66.

Owen, P.R., "Computational Simulation of Unsteady Flow in a Transonic Compressor Rotor", 1986, 189.

Paduano, J.D., "Active Control of Rotating Stall in Axial Compressors", 1992, 208.

Peterson, C.R., "Boundary Layer on an Airfoil in a Cascade", 1958, 49.

Phillips, M.S., "Role of Flow Alignment and Inlet Blockage on Vaned Diffuser Performance", 1997, 229.

Prell, M.E., "An Experimental Investigation of Stator Hub Treatment in an Axial Flow Compressor", 1981, 161.

Probst, H.C., Oliver, D.A., "The Display of Multi-Dimensionl Flows in Turbomachinery", 1972, 111.

Qvale, E.B., "A Study of Outlet Guide Vanes", 1963, 72.

Roberts, R., "A Light Scattering Investigation of Droplet Growth in Nozzle Condensation", 1969, 97.

Ryan, F.J., Ohashi, H., "The Effect of Tip Clearance on the Performance of an Axial Flow Fan", 1955, 31.

Sandler, S.B., "Experimental Determination of Volute Effects on the Stability of Low Specific Speed Centrifugal Pumps", 1992, 212.

Saxer, A.P., "A Numerical Analysis of 3-D Inviscid Stator/Rotor Interactions Using non-Reflecting Boundary Conditions", 1992, 209.

Schaffner, J.E., Ingard, K.U., "Sound Generation from a Transonic Compressor Stage", 1981, 160.

Schaub, U.W., "The Behavior of a Wake in an Adverse Pressure Gradient", 1961, 62.

Schneider, K.H., "Potential Flow Through a Cascade of Known Airfoils", 1955, 32.

Schneider, K.H., "Boundary Layer Effects on Airfoil Lift", 1958, 47.

Schwind, R.G., "The Three-Dimensional Boundary Layer Near a Strut", 1962, 67.

Sehra, A.K., "Boundary Layer and Wake Modifications to Compressor Design Systems: The Effect of Blade-to-Blade Flow Variations on the Mean Flow Field of a Transonic Rotor", 1979, 144A.

Seidel, B.S., "Asymmetric Inlet Flow in Axial Turbo Machines", 1959, 51.

Senoo, Y., "The Boundary Layer on the End Wall of a Turbine Nozzle Cascade", 1956, 35.

Senoo, Y., "Three-Dimensional Laminar Boundary Layer in Curved Channels with Acceleration", 1956, 37.

Senoo, Y., Taylor, E.S., Batra, S., Hinck, E., "Control of Wall Boundary Layer in an Axial Compressor", 1990, 59.

Silkowski, P.D., "Measurements of Rotor Stalling in a Matched and a Mismatched Multistage Compressor", 1995, 221.

Simon, J., "Feedback Stabilization of Compression Systems", 1993, 216.

Shin, H.W., Shippee, C., "Quantitative Investigation of Inlet Vortex Flow Field", 1984, 179.

So, K.L, "Vortex Decay in a Conical Diffuser", 1964, 75.

Soderberg, O., "Secondary Flow and Losses in a Compressor Cascade", 1958, 46.

Stenning, A.H., "Stall Propagation in a Cascade of Airfoils", 1954, 25.

Stenning, A.H., "Stall Propagation in Axial Compressors", 1955, 28.

Stenning, A.H., Seidel, B.S., Senoo, Y., "Stall Propagation in a Cascade of Airfoils" (final report), 1957, 41.

Stenning, A.H., "The Design of Axial Inducers for Turbopumps", 1958, 44.

Stephens, H.E. III, "Wake Behavior Downstream of a Transonic Compressor Rotor", 1974, 118.

Stewart, C.C.,"A Comparison of Turbulent Boundary Layer Theories" 1960, 57.

Sturek, W.B., "Temperature Wake in an Adverse Pressure Gradient", 1961, 64.

Succi, G.P., "The Interaction of Sound with Turbulent Flow", 1977, 140.

Succi, G.P., "Noise and Performance of Propellers for Light Aircraft" (Final Report NASA Contract NAS1-15154, 2/24/78-7/31/80), 1980, 154.

Tan, C.S. "Three-Dimensional Incompressible and Compressible Beltrami Flow Through a Highly-Loaded Isolated Rotor", 1979, 147.

Tan, C.S., "Three-Dimensional Vorticity-Induced Flow Effects in Highly-Loaded Axial Compressors", 1980, 141.

Tan, C.S. "Asymmetric Inlet Flows Through Axial Compressors", 1980, 151.

Tan, C.S., "An Experimental Study of the Effects of Swirl and Density Difference on Mixing in Shear Flows", 1980, 153.

Tan, C.S., Wang, C., McCune, J.E., Hawthorne, W.R., "Three-Dimensional Blade Design for Large Deflections Using an Analytic Theory", 1982, 168.

Tan, C.S., Greitzer, E.M., "Non-Axisymmetric Compressorible Flow Through Annular Actuator Disks", 1982, 169.

Taylor, E.S., Dean, R.C., "A Survey of Research Activities During 1953-54 and Proposals for Research During 1955", 1954, 26.

Taylor, E.S., Stevenson, R., Dean, R.C. Jr., "The Control of Secondary Flow in the Wall Boundary Layers of Axial Turbomachines", 1954, 27-4.

Taylor, E.S., "Boundary Layers, Wakes and Losses in Turbomachines", 1971, 105.

Thompkins, W.T. Jr., Kerrebrock, J.L., "Exit Flow from a Transonic Compressor Rotor", 1975, 123.

Thompkins, W.T. Jr., "An Experimental and Computational Study of the Flow in a Transonic Compressor Rotor", 1976, 129.

Thompkins, W. T. Jr., "A Fortran Program for Calculating Three-Dimensional, Inviscid, Rotational Flows with Shock Waves in Axial Compressor Blade Rows, I–User’s Manual", 1981, 162.

Turner, J.R., "An Investigation of the End-Wall Boundary Layer of a Turbine Nozzle Cascade", 1955, 30.

Turner, M.G., "Design and Analysis of Internal Flowfields Using a Two-Stream Function Formulation", 1990, 201.

Usab W.J. Jr.,"Prediction of Three-Dimensional Compressible Turbulent Boundary Layers on Transonic Compressor Blades", 1980, 152.

Valkov, T., "Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes", 1993, 215.

Valkov, T., "The Effect of Upstream Rotor Vortical Disturbances on the Time-Average Performance of Axial Compressor Stators", 1997, 227.

Van Schalkwyk, C.M. , "Active Control of Rotating Stall with Inlet Distortion" , 1996, 222.

Viguier, H.C., "A Secondary Flow Approach to the Inlet Vortex Flow Field", 1980, 155.

Weigl, H.J., "Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor", 1997, 226.

Yang, Y.L, Tan, C.S., Hawthorne, W.R., "Aerodynamic Design of Turbomachinery Blading in Three-Dimensional Flow: An Application to Radial Inflow Turbines", 1991, 204.

Yokoyama, E., "Comparative Study of Tip Clearance Effects in Compressors and Turbine", 1961, 63.

Youngren, H.H., "Analysis and Design of Transonic Cascades with Splitter Vanes", 1991, 203.

back to top