1. Film cooling with injection through a circular hole;Goldstein;J. Engng Pwr,1968
2. Film cooling following injection through inclined circular tubes;Goldstein;NASA CR72612,1969
3. Prediction of effects of mass transfer cooling on the blade row efficiency of turbine aerofoils;Hartsel;AIAA No. 72-11,1972
4. Effects of hole geometry and density on three-dimensional film cooling;Goldstein;Int. J. Heat Mass Transfer,1974
5. Film cooling measurements;Kruse;DEVLR Report No. 352-74/9,1974