Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler (NASA/TM ; 208146)
Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler
原資料の出版事項: [Washington, D.C. ; Springfield, Va. : National Aeronautics and Space Administration : National Technical Information Service, distributor, 1997]