Volume 110 Issue 3 | J. Turbomach. | ASME Digital Collection

Research Papers

Development, Testing, and Performance Prediction of Radial Compressor Stages for Multistage Industrial Compressors

J. Turbomach. July 1988, 110(3): 283–292. doi: https://doi.org/10.1115/1.3262194

View articletitled, Development, Testing, and Performance Prediction of Radial Compressor Stages for Multistage Industrial Compressors

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Topics: Compressors , Testing , Computational methods , Design methodology , Dimensional analysis , Interpolation , Reynolds number

Unsteady Flow in a Centrifugal Compressor With Different Types of Vaned Diffusers

U. Haupt, U. Seidel, A. N. Abdel-Hamid, M. Rautenberg

J. Turbomach. July 1988, 110(3): 293–302. doi: https://doi.org/10.1115/1.3262195

Abstract

View articletitled, Unsteady Flow in a Centrifugal Compressor With Different Types of Vaned Diffusers

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Topics: Compressors , Diffusers , Unsteady flow , Flow (Dynamics) , Pressure , Blades , Fluctuations (Physics) , Impellers , Oscillations , Surges

Application of Viscous Flow Computations for the Aerodynamic Performance of a Backswept Impeller at Various Operating Conditions

C. Hah, A. C. Bryans, Z. Moussa, M. E. Tomsho

J. Turbomach. July 1988, 110(3): 303–311. doi: https://doi.org/10.1115/1.3262196

Abstract

View articletitled, Application of Viscous Flow Computations for the Aerodynamic Performance of a Backswept Impeller at Various Operating Conditions

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Topics: Computation , Impellers , Viscous flow , Design , Engineering systems and industry applications , Flow (Dynamics) , Surges

Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry

K.-D. Broichhausen, H. E. Gallus, R. Mo¨nig

J. Turbomach. July 1988, 110(3): 312–321. doi: https://doi.org/10.1115/1.3262197

Abstract

View articletitled, Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry

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Topics: Compressors , Design , Geometry , Flow (Dynamics) , Rotors , Stators , Axial flow , Boundary layers , Computational methods , Computers

Experimental Investigations of Flows Through a Plane Cascade at Large Angles of Attack With Separations

Chuan-Gang Gu, Lai-Qin Luo, Yong-Miao Miao

J. Turbomach. July 1988, 110(3): 323–328. doi: https://doi.org/10.1115/1.3262200

Abstract

View articletitled, Experimental Investigations of Flows Through a Plane Cascade at Large Angles of Attack With Separations

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Topics: Cascades (Fluid dynamics) , Flow (Dynamics) , Blades , Wire , Flow visualization , Pressure , Separation (Technology) , Signals , Stress , Turbulence

Interaction Mechanisms Between Tip Leakage Flow and the Passage Vortex in a Linear Turbine Rotor Cascade

A. Yamamoto

J. Turbomach. July 1988, 110(3): 329–338. doi: https://doi.org/10.1115/1.3262201

Abstract

View articletitled, Interaction Mechanisms Between Tip Leakage Flow and the Passage Vortex in a Linear Turbine Rotor Cascade

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Topics: Cascades (Fluid dynamics) , Leakage flows , Rotors , Turbines , Vortices , Flow (Dynamics) , Clearances (Engineering) , Flow visualization , Flowmeters , Leakage

Navier–Stokes Solution for Steady Two-Dimensional Transonic Cascade Flows

O. K. Kwon

J. Turbomach. July 1988, 110(3): 339–346. doi: https://doi.org/10.1115/1.3262202

Abstract

View articletitled, Navier–Stokes Solution for Steady Two-Dimensional Transonic Cascade Flows

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Topics: Cascades (Fluid dynamics) , Flow (Dynamics) , Navier-Stokes equations , Turbines , Turbulence

Shock Embedding Discontinuous Solution of Elliptic Equation for Inverse Problem of Transonic S₂ Flow

Hongji Chen, Chung-Hua Wu

J. Turbomach. July 1988, 110(3): 347–353. doi: https://doi.org/10.1115/1.3262203

Abstract

View articletitled, Shock Embedding Discontinuous Solution of Elliptic Equation for Inverse Problem of Transonic <em>S</em><sub>2</sub> Flow

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Topics: Flow (Dynamics) , Inverse problems , Shock (Mechanics) , Computers , Transonic flow , Algorithms , Compressors , Computation , Fittings , Rotors

The Design of Shock-Free Compressor Cascades Including Viscous Boundary-Layer Effects

A. A. Hassan

J. Turbomach. July 1988, 110(3): 354–362. doi: https://doi.org/10.1115/1.3262204

Abstract

View articletitled, The Design of Shock-Free Compressor Cascades Including Viscous Boundary-Layer Effects

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Topics: Boundary layers , Compressors , Design , Shock (Mechanics) , Algorithms , Blades , Flow (Dynamics) , Turbulence , Airfoils , Clearances (Engineering)

Numerical Computation of Nonisentropic Potential Equations for Transonic Cascade Flows

J. Z. Xu, J. Y. Du, W. Y. Ni

J. Turbomach. July 1988, 110(3): 363–368. doi: https://doi.org/10.1115/1.3262205

Abstract

View articletitled, Numerical Computation of Nonisentropic Potential Equations for Transonic Cascade Flows

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Topics: Cascades (Fluid dynamics) , Computation , Flow (Dynamics) , Density , Entropy , Momentum , Shock (Mechanics) , Boundary-value problems , Temperature

Inter and Intrablade Row Laser Velocimetry Studies of Gas Turbine Compressor Flows

M. C. Williams

J. Turbomach. July 1988, 110(3): 369–376. doi: https://doi.org/10.1115/1.3262206

Abstract

View articletitled, Inter and Intrablade Row Laser Velocimetry Studies of Gas Turbine Compressor Flows

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Topics: Compressors , Flow (Dynamics) , Gas turbines , Laser velocimetry , Data acquisition systems , Instrumentation , NASA , Aerodynamics , Lasers , Resolution (Optics)

Laser-Doppler Velocimeter Measurement of Annulus Wall Boundary Layer Development in a Compressor Rotor

B. Lakshminarayana, K. N. S. Murthy

J. Turbomach. July 1988, 110(3): 377–385. doi: https://doi.org/10.1115/1.3262207

Abstract

View articletitled, Laser-Doppler Velocimeter Measurement of Annulus Wall Boundary Layer Development in a Compressor Rotor

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Topics: Annulus , Boundary layers , Compressors , Lasers , Rotors , Velocimeters , Blades , Leakage flows , Flow (Dynamics) , Probes

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

D. C. Rabe, A. J. Wennerstrom, W. F. O’Brien

J. Turbomach. July 1988, 110(3): 386–392. doi: https://doi.org/10.1115/1.3262208

Abstract

View articletitled, Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

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Topics: Boundary layers , Compressors , Rotors , Shock waves , Blades , Lasers , Air Force , Chords (Trusses) , Flow (Dynamics) , Shear (Mechanics)

The Use of Holographic Interferometry for Turbomachinery Fan Evaluation During Rotating Tests

R. J. Parker, D. G. Jones

J. Turbomach. July 1988, 110(3): 393–400. doi: https://doi.org/10.1115/1.3262209

Abstract

View articletitled, The Use of Holographic Interferometry for Turbomachinery Fan Evaluation During Rotating Tests

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Topics: Blades , Boundary layers , Computer simulation , Design , Flow (Dynamics) , Flow visualization , Flutter (Aerodynamics) , Holographic interferometry , Holography , Leakage

A Full Quasi-Three-Dimensional Calculation of Flow in Turbomachines

M. Ribaut

J. Turbomach. July 1988, 110(3): 401–404. doi: https://doi.org/10.1115/1.3262210

Abstract

View articletitled, A Full Quasi-Three-Dimensional Calculation of Flow in Turbomachines

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Topics: Flow (Dynamics) , Turbomachinery , Blades , Boundary-value problems , Vorticity

Calculation of Turbulent Flow and Heat Transfer in Channels With Streamwise-Periodic Flow

M. A. Habib, A. E. Attya, D. M. McEligot

J. Turbomach. July 1988, 110(3): 405–411. doi: https://doi.org/10.1115/1.3262211

Abstract

View articletitled, Calculation of Turbulent Flow and Heat Transfer in Channels With Streamwise-Periodic Flow

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Topics: Flow (Dynamics) , Heat transfer , Turbulence , Computational methods , Energy dissipation , Heat losses , Kinetic energy , Momentum , Stress

Influence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes

V. Krishnamoorthy, B. R. Pai, S. P. Sukhatme

J. Turbomach. July 1988, 110(3): 412–416. doi: https://doi.org/10.1115/1.3262212

Abstract

View articletitled, Influence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes

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Topics: Flow (Dynamics) , Heat transfer , Nozzle guide vanes , Cascades (Fluid dynamics) , Turbulence , Combustion chambers , Temperature , Blades , Heat flux , Temperature distribution

Discussions

Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

R. Fuchs, H. Starken

J. Turbomach. July 1988, 110(3): 321–322. doi: https://doi.org/10.1115/1.3262198

View articletitled, Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

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Topics: Compressors , Design , Geometry

Closure to “Discussion of ‘Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry’” (1988, ASME J. Turbomach., 110, pp. 321–322)

K.-D. Broichhausen, H. E. Gallus, R. Mo¨nig

J. Turbomach. July 1988, 110(3): 322. doi: https://doi.org/10.1115/1.3262199

View articletitled, Closure to “Discussion of ‘Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry’” (1988, ASME J. Turbomach., 110, pp. 321–322)

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Topics: Compressors , Design

Technical Briefs

The Effect of Hub Radius on the Flow Due to a Rotating Disk

John W. Chew

J. Turbomach. July 1988, 110(3): 417–418. doi: https://doi.org/10.1115/1.3262213

View articletitled, The Effect of Hub Radius on the Flow Due to a Rotating Disk

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Topics: Flow (Dynamics) , Rotating disks

Research Papers

Development, Testing, and Performance Prediction of Radial Compressor Stages for Multistage Industrial Compressors

Unsteady Flow in a Centrifugal Compressor With Different Types of Vaned Diffusers

Application of Viscous Flow Computations for the Aerodynamic Performance of a Backswept Impeller at Various Operating Conditions

Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry

Experimental Investigations of Flows Through a Plane Cascade at Large Angles of Attack With Separations

Interaction Mechanisms Between Tip Leakage Flow and the Passage Vortex in a Linear Turbine Rotor Cascade

Navier–Stokes Solution for Steady Two-Dimensional Transonic Cascade Flows

Shock Embedding Discontinuous Solution of Elliptic Equation for Inverse Problem of Transonic S₂ Flow

The Design of Shock-Free Compressor Cascades Including Viscous Boundary-Layer Effects

Numerical Computation of Nonisentropic Potential Equations for Transonic Cascade Flows

Inter and Intrablade Row Laser Velocimetry Studies of Gas Turbine Compressor Flows

Laser-Doppler Velocimeter Measurement of Annulus Wall Boundary Layer Development in a Compressor Rotor

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

The Use of Holographic Interferometry for Turbomachinery Fan Evaluation During Rotating Tests

A Full Quasi-Three-Dimensional Calculation of Flow in Turbomachines

Calculation of Turbulent Flow and Heat Transfer in Channels With Streamwise-Periodic Flow

Influence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes

Discussions

Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

Closure to “Discussion of ‘Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry’” (1988, ASME J. Turbomach., 110, pp. 321–322)

Technical Briefs

The Effect of Hub Radius on the Flow Due to a Rotating Disk

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