Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours

Bholanath Behera,; K. Srinivasan,

doi:10.1515/TJJ.2007.24.2.115

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Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours

Bholanath Behera, and K. Srinivasan,

Published/Copyright: June 1, 2007

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From the journal International Journal of Turbo and Jet Engines Volume 24 Issue 2

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Harvard
Chicago
Vancouver

Behera,, Bholanath and Srinivasan,, K.. "Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours" International Journal of Turbo and Jet Engines, vol. 24, no. 2, pp. 115-118. https://doi.org/10.1515/TJJ.2007.24.2.115

Behera,, B. & Srinivasan,, K. (). Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours. International Journal of Turbo and Jet Engines, 24(2), 115-118. https://doi.org/10.1515/TJJ.2007.24.2.115

Behera,, B. and Srinivasan,, K. () Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 2), pp. 115-118. https://doi.org/10.1515/TJJ.2007.24.2.115

Behera,, Bholanath and Srinivasan,, K.. "Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours" International Journal of Turbo and Jet Engines 24, no. 2 (): 115-118. https://doi.org/10.1515/TJJ.2007.24.2.115

Behera, B, Srinivasan, K. Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours. International Journal of Turbo and Jet Engines. ;24(2): 115-118. https://doi.org/10.1515/TJJ.2007.24.2.115

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Published Online: 2007-06

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Articles in the same Issue

CONTENTS
Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
Numerical Studies of a Novel Vortex Combustor

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https://doi.org/10.1515/TJJ.2007.24.2.115

Articles in the same Issue

CONTENTS
Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
Numerical Studies of a Novel Vortex Combustor