Considerations of Turbine Cooling Systems for Mach 3 Flight

Preliminary Investigation of Catastrophic Fracture of Liquid- Filled Tanks Impacted by High-velocity Particles

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

Investigation of Damage to Brittle Materials by Impact with High-velocity Projectiles Into Glass and Lucite

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

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