Navier-Stokes analysis of turbomachinery blade external heat transfer

Author Information:

Ameri, A. A.; Sockol, P. M.; Gorla, R. S. R.

Abstract:

The two-dimensional, compressible, thin-layer Navier-Stokes and energy equations were solved numerically to obtain heat transfer rates on turbomachinery blades. The Baldwin-Lomax algebraic model and the q - omega low Reynolds number, two-equation model were used for modeling of turbulence. For the numerical solution of the governing equations a four-stage Runge-Kutta solver was employed. The turbulence model equations were solved using an implicit scheme. Numerical solutions are presented for two-dimensional flow within two vane cascades. The heat transfer results and the pressure distributions were compared with published experimental data. The agreement between the numerical calculations and the experimental values were found to be generally favorable. The position of transition from laminar to turbulent flow was also predicted accurately.

Publication Date:

Apr 1, 1992

Document ID (CASI):

19920045894

Grant Number:

NAG3-548

Accession Number:

92A28518

Security Classif.:

Unclassified

Restriction on Access:

Unlimited

Authorized Users:

Publicly available

Copyright Indicator:

Copyright

Description:

8p

Source Publication:

Journal of Propulsion and Power (ISSN 0748-4658) / 8; 374-381

Imprint and Other Notes:

Journal of Propulsion and Power (ISSN 0748-4658), vol. 8, Mar.-Apr. 1992, p. 374-381.

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