1. Abu-Ghannam
B. J.
, and ShawR., 1980, “Natural transition of boundary layers—The effect of turbulence, pressure gradient, and flow history,” J. Mechanical Engineering Science, Vol. 22, No. 5, pp. 213–228.
2. Arts, T., Lambert de Rouvroit, M., and Sieverding, C. H., 1989, “Contribution to the workshop on two-dimensional inviscid and viscous turbomachinery flow calculation,” Numerical Methods for Flows in Turbomachinery, VKI Lecture Series 1989-06.
3. Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, “Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade,” VKI Technical Note 174.
4. Arts, T., 1994, “Test case No 2: highly loaded transonic and film cooled linear turbine guide vane cascade LS94,” Numerical Methods for Flow Calculations in Turbomachines, VKI Lecture Series 1994-06.
5. Billonnet, G., Fourmaux, A., Huard, J., and Occhionigro, A., 1995, “Utilisation de calculs 2.5D et 3D d’ e´coulements instationnaires pour le choix de l’instrumentation d’un banc d’essai de turbine,” 85th PEP-AGARD Loss and Unsteady Flows in Turbomachines, Derby, UK.