Effects of Pressure Mismatch on Slot Injection in Supersonic Flow

J.A. Schetz,; F.S. Bitlig,; S. Favin,; H.E. Gilreath,

doi:10.1515/TJJ.1992.9.2.135

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Effects of Pressure Mismatch on Slot Injection in Supersonic Flow

J.A. Schetz, , F.S. Bitlig, , S. Favin, and H.E. Gilreath,

Published/Copyright: June 1, 1992

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From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 2

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Harvard
Chicago
Vancouver

Schetz,, J.A., Bitlig,, F.S., Favin,, S. and Gilreath,, H.E.. "Effects of Pressure Mismatch on Slot Injection in Supersonic Flow" International Journal of Turbo and Jet Engines, vol. 9, no. 2, pp. 135-146. https://doi.org/10.1515/TJJ.1992.9.2.135

Schetz,, J., Bitlig,, F., Favin,, S. & Gilreath,, H. (). Effects of Pressure Mismatch on Slot Injection in Supersonic Flow. International Journal of Turbo and Jet Engines, 9(2), 135-146. https://doi.org/10.1515/TJJ.1992.9.2.135

Schetz,, J., Bitlig,, F., Favin,, S. and Gilreath,, H. () Effects of Pressure Mismatch on Slot Injection in Supersonic Flow. International Journal of Turbo and Jet Engines, Vol. 9 (Issue 2), pp. 135-146. https://doi.org/10.1515/TJJ.1992.9.2.135

Schetz,, J.A., Bitlig,, F.S., Favin,, S. and Gilreath,, H.E.. "Effects of Pressure Mismatch on Slot Injection in Supersonic Flow" International Journal of Turbo and Jet Engines 9, no. 2 (): 135-146. https://doi.org/10.1515/TJJ.1992.9.2.135

Schetz, J, Bitlig, F, Favin, S, Gilreath, H. Effects of Pressure Mismatch on Slot Injection in Supersonic Flow. International Journal of Turbo and Jet Engines. ;9(2): 135-146. https://doi.org/10.1515/TJJ.1992.9.2.135

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Published Online: 1992-06

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Articles in the same Issue

CONTENTS
The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
Shock Wave/Free Shear Layer Interaction
Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method

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https://doi.org/10.1515/TJJ.1992.9.2.135

Articles in the same Issue

CONTENTS
The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
Shock Wave/Free Shear Layer Interaction
Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method