Search U.S. government technical reports digitized or harvested by TRAIL.
Development of a Laminar Boundary Layer Behind a Suction Point
Generalized Theory for Seaplane Impact
Concerning the Flow About Ring-Shaped Cowlings of Finite Thickness: Part 1
Concerning the Flow About Ring-Shaped Cowlings Part 8: Further Measurements on Annular Profiles
On a Solution of the Nonlinear Differential Equation for Transonic Flow Past a Wave-Shaped Wall
The Structure of Turbulence in Fully Developed Pipe Flow
On the Development of Turbulent Wakes From Vortex Streets
Relation Between Roughness of Interface and Adherence of Porcelain Enamel to Steel
Experimental Aerodynamic Derivatives of a Sinusoidally Oscillating Airfoil in Two-Dimensional Flow
Preliminary Investigation of a New Type of Supersonic Inlet
The Ames Supersonic Free-Flight Wind Tunnel
Supplementary Bibliography of NACA Reports Related to Instrumentation and Research Techniques
A Method for Estimating Speed Response of Gas-Turbine Engines
Dynamic Response of Turbine-Blade Temperature to Exhaust-Gas Temperature for Gas-Turbine Engines
Development of a Laminar Boundary Layer Behind a Suction Point
Boundary-Layer Measurements on Several Porous Materials With Suction Applied
On the Design of Airfoils in Which the Transition of the Boundary Layer Is Delayed
Comparison of Three Multicylinder Icing Meters and Critique of Multicylinder Method
A Study of Poisson's Ratio in the Yield Region
A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diagram
Investigation of the Structural Damping of a Full-Scale Airplane Wing
Fatigue Strengths of 14S-T4 Aluminum Alloy Subjected to Biaxial Tensile Stresses
Equal-Strength Design of Tension-Field Webs and Uprights
Theory of Supersonic Potential Flow in Turbomachines
Fatigue and Static Tests of Flush-Riveted Joints
Direct Measurements of Skin Friction
Hydrodynamic Characteristics of a Low-Drag, Planing-Tail Flying Boat Hull
Laminar Boundary Layer Over Flat Plate in a Flow Having Circular Streamlines
Normal Accelerations and Operating Conditions Encountered by a Helicopter in Air-Mail Operations