Considerations of Turbine Cooling Systems for Mach 3 Flight

Projectile-impact-induced Fracture of Liquid-filled, Filament-reinforced Plastic Or Aluminum Tanks: Volume 3456

Experimental and Analytical Investigation of Heat-transfer Characteristics of a Return-flow Air-cooled Turbine Rotor Blade

NACA Research Memorandum: Issue 58, Volume 67

NACA Research Memorandum: Issue 58, Volume 67

Experimental Investigation of Metal Temperatures of Air-cooled Airfoil Leading Edges at Subsonic Flow and Gas Temperatures Up to 2780 Degrees F

Experimental and Analytical Investigation of Heat-transfer Characteristics of a Return-flow Air-cooled Turbine Rotor Blade

Analytical and Experimental Investigation of a Forced-convection Air-cooled Internal Strut-supported Turbine Blade

Preliminary Survey of Possible Cooling Methods for Hypersonic Aircraft

Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel

Fabrication and Endurance of Air-cooled Strut-supported Turbine Blades with Struts Cast of X-40 Alloy

Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine: Endurance evaluation of shell-supported turbine rotor blades made of timken 17-22A (S) steel, Part 14