Volume 10, Issue 2 No AccessRole of mainstream flow velocity in film cooling in a ductShyang-Lin Kuo, Neng-Li Zhang and Wen-Jei YangShyang-Lin Kuo General Motors Corporation, Warren, Michigan 48090Search for more papers by this author, Neng-Li Zhang University of Michigan, Ann Arbor, Michigan 48109Search for more papers by this author and Wen-Jei Yang University of Michigan, Ann Arbor, Michigan 48109Search for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/3.800SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article FiguresReferencesRelatedDetailsSee PDF for referencesCited byEnhancement of Film Cooling Effectiveness in a Supersonic Nozzle10 March 2023 | Entropy, Vol. 25, No. 3Review on film cooling of liquid rocket enginesPropulsion and Power Research, Vol. 7, No. 1Effect of continuous or discrete shock wave generators on supersonic film coolingInternational Journal of Heat and Mass Transfer, Vol. 108Effect of injector configuration in rocket nozzle film cooling21 May 2015 | Heat and Mass Transfer, Vol. 52, No. 4Role of gaseous film cooling injector orientation in duct flow: Experimental StudyInternational Communications in Heat and Mass Transfer, Vol. 48Internal wall-jet film cooling with compound angle cylindrical holesEnergy Conversion and Management, Vol. 68Internal Wall-Jet Film Cooling with Straight Cylindrical Holes S. R. Shine , S. Sunil Kumar and B. N. Suresh 6 September 2013 | Journal of Thermophysics and Heat Transfer, Vol. 26, No. 3Heat transfer — a review of 1996 literatureInternational Journal of Heat and Mass Transfer, Vol. 43, No. 8 What's Popular Volume 10, Number 2April 1996 Metrics Crossmark TopicsAerodynamicsAerospace SciencesBoundary LayersFlow RegimesFluid DynamicsFluid MechanicsNormal Shock WaveOblique Shock WaveShock WavesVortex DynamicsWind Tunnels KeywordsMainstream FlowFilm CoolingMach NumbersMass Flow RateFlow VisualizationHeat TransferVortex SheddingJet NozzleSupersonic Wind TunnelsAcoustic MeasurementDigital Published online23 May 2012