Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine

Journal of Propulsion and Power

Volumn 6, Issue 3, 1990, Pages 276-282

  Rai, Man Mohan ^a   Dringt, Robert P ^b,c  

^a NASA AMES RESEARCH CENTER   (United States)

^b UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^c Gas Turbine Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85002886228     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.25431     Document Type: Article

References (12)

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2. Munk, M, and Prim, R. C, “On the Multiplicity of Steady Gas Flows Having the Same Streamline Pattern,” Proceedings of the National Academy of Sciences, Vol. 33, 1947.
3. Hawthorne, W. R, “Secondary Vorticity in Stratified Compressible Fluids in Rotating Systems,” Univ. of Cambridge, Cambridge, UK, Dept, of Engineering Rept. CUED/A-Turbo/TR 63, 1974.
4. Lakshminarayana, B, “Effects of Inlet Temperature Gradients on Turbomachinery Performance,”ASME Journal of Engineering for Power, Vol. 97, No. 1, Jan. 1975, pp. 64-74.
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8. Baldwin, B. S, and Lomax, H, “Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow,” AIAA Paper 78257, Jan. 1978.
9. Dring, R. P, Joslyn, H. D, Hardin, L. W, and Wagner, J. H, “Turbine Rotor-Stator Interaction,” Journal of Engineering for Power, Vol. 104, Oct. 1982.
10. Rai, M. M, and Chaussee, D. S, “New Implicit Boundary Procedures: Theory and Application,”AIAA Journal, Vol. 22, No. 8, Aug. 1984, pp. 1094-1100.
11. Rai, M. M, “Three-Dimensional Navier-Stokes Simulations of Turbine Rotor-Stator Interaction, Part 2-Results,” Journal of Propulsion and Power, Vol. 5, No. 3, May-June 1989, pp. 312-319.
12. Schlichting, H, Boundary Layer Theory, 6th ed, McGraw-Hill, New York, 1968, pp. 27-34.