Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet

W.H. Lai,; W. Huang,; T.L. Jiang,

doi:10.1515/TJJ.1998.15.3.155

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Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet

W.H. Lai, , W. Huang, and T.L. Jiang,

Published/Copyright: September 1, 1998

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From the journal International Journal of Turbo and Jet Engines Volume 15 Issue 3

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APA
Harvard
Chicago
Vancouver

Lai,, W.H., Huang,, W. and Jiang,, T.L.. "Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet" International Journal of Turbo and Jet Engines, vol. 15, no. 3, pp. 155-164. https://doi.org/10.1515/TJJ.1998.15.3.155

Lai,, W., Huang,, W. & Jiang,, T. (). Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet. International Journal of Turbo and Jet Engines, 15(3), 155-164. https://doi.org/10.1515/TJJ.1998.15.3.155

Lai,, W., Huang,, W. and Jiang,, T. () Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet. International Journal of Turbo and Jet Engines, Vol. 15 (Issue 3), pp. 155-164. https://doi.org/10.1515/TJJ.1998.15.3.155

Lai,, W.H., Huang,, W. and Jiang,, T.L.. "Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet" International Journal of Turbo and Jet Engines 15, no. 3 (): 155-164. https://doi.org/10.1515/TJJ.1998.15.3.155

Lai, W, Huang, W, Jiang, T. Effects of Orifice Size and Impinging Angle on the Characteristics of a Like-Doublet Impinging-Jet. International Journal of Turbo and Jet Engines. ;15(3): 155-164. https://doi.org/10.1515/TJJ.1998.15.3.155

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Published Online: 1998-09

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Articles in the same Issue

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.1998.15.3.155

Articles in the same Issue

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