1. The turbulent wall jet;Prog. Aerosp. Sci.,1979
2. Flowfield measurements for film-cooling holes with expanded exits,1996
3. G. J.
Sturgess
, “
Wall cooling by gaseous injection for a high-performance combustion system,” Ph.D. thesis (
Loughborough University, 1971).
4. D.
Singelmann
and
H.Mueller, “
BMW rocket-engine development,” Technical Report No. F-TR-2201-ND (
Air Materiel Command Wright-Patterson,
AFB, OH, 1948).
5. E.
Förthmann
, “Turbulent Jet Expansion,” Report No. NACA TM-789, 1936.