Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation

K.C. Chang,; C.S. Chen,

doi:10.1515/TJJ.1991.8.3-4.157

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Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation

K.C. Chang, and C.S. Chen,

Published/Copyright: December 1, 1991

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From the journal International Journal of Turbo and Jet Engines Volume 8 Issue 3-4

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Chang,, K.C. and Chen,, C.S.. "Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation" International Journal of Turbo and Jet Engines, vol. 8, no. 3-4, pp. 157-184. https://doi.org/10.1515/TJJ.1991.8.3-4.157

Chang,, K. & Chen,, C. (). Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation. International Journal of Turbo and Jet Engines, 8(3-4), 157-184. https://doi.org/10.1515/TJJ.1991.8.3-4.157

Chang,, K. and Chen,, C. () Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation. International Journal of Turbo and Jet Engines, Vol. 8 (Issue 3-4), pp. 157-184. https://doi.org/10.1515/TJJ.1991.8.3-4.157

Chang,, K.C. and Chen,, C.S.. "Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation" International Journal of Turbo and Jet Engines 8, no. 3-4 (): 157-184. https://doi.org/10.1515/TJJ.1991.8.3-4.157

Chang, K, Chen, C. Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation. International Journal of Turbo and Jet Engines. ;8(3-4): 157-184. https://doi.org/10.1515/TJJ.1991.8.3-4.157

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Published Online: 1991-12

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Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula

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https://doi.org/10.1515/TJJ.1991.8.3-4.157

Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula