Survey of advantages and problems associated with transpiration cooling and film cooling of gas-turbine blades
Publisher: NACA
Published: 1951
Place of publication: Washington, D.C.
Language: eng
Number of pages: 42
Subjects: Turbines--Blades--Research; Airplanes--Motors--Cooling; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003810653&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003810653&ix=nu&I=0&V=D&pm=1</a>