Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude I : liquid-cooling systems

Author:	Schramm, Wilson B
Additional Authors:	Nachtigall, Alfred J
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52J29
Link:	https://digital.library.unt.edu/ark:/67531/metadc59434/