Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine

A.W. Smith,; N. Ramachandran,

doi:10.1515/TJJ.1998.15.3.175

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Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine

A.W. Smith, und N. Ramachandran,

Veröffentlicht/Copyright: 1. September 1998

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 15 Heft 3

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MLA
APA
Harvard
Chicago
Vancouver

Smith,, A.W. and Ramachandran,, N.. "Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine" International Journal of Turbo and Jet Engines, vol. 15, no. 3, pp. 175-186. https://doi.org/10.1515/TJJ.1998.15.3.175

Smith,, A. & Ramachandran,, N. (). Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine. International Journal of Turbo and Jet Engines, 15(3), 175-186. https://doi.org/10.1515/TJJ.1998.15.3.175

Smith,, A. and Ramachandran,, N. () Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine. International Journal of Turbo and Jet Engines, Vol. 15 (Issue 3), pp. 175-186. https://doi.org/10.1515/TJJ.1998.15.3.175

Smith,, A.W. and Ramachandran,, N.. "Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine" International Journal of Turbo and Jet Engines 15, no. 3 (): 175-186. https://doi.org/10.1515/TJJ.1998.15.3.175

Smith, A, Ramachandran, N. Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine. International Journal of Turbo and Jet Engines. ;15(3): 175-186. https://doi.org/10.1515/TJJ.1998.15.3.175

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Published Online: 1998-09

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Artikel in diesem Heft

CONTENTS
Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet
Optimal Inverse Analysis of Vectored Thrust Maneuvering
Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine
LDV Measurements of a Mixed-Flow Impeller at Design and Near Stall
Incipient Stall Mean Flow and Subsequent Rotating Stall in a Mixed Flow Centrifugal Compressor
Fuel-Air Mixing in Solid Fuel Scramjet Combustors

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https://doi.org/10.1515/TJJ.1998.15.3.175

Artikel in diesem Heft

CONTENTS
Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet
Optimal Inverse Analysis of Vectored Thrust Maneuvering
Two-Dimensional LDV Measurements In The Inlet And Exit Manifolds Of A Single Stage Oxidizer Turbine
LDV Measurements of a Mixed-Flow Impeller at Design and Near Stall
Incipient Stall Mean Flow and Subsequent Rotating Stall in a Mixed Flow Centrifugal Compressor
Fuel-Air Mixing in Solid Fuel Scramjet Combustors