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Decade:
1950-1959 (1)
1940-1949 (334)
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NACA Wartime Reports (334)
NACA Memorandum Report (2)
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Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body : NACA model 84 series
Aerodynamic tests of a full-scale TBF-1 aileron installation in the Langley 16-foot high-speed tunnel
Airfoil-contour modifications based on (epsilon)-curve method of calculating pressure distribution
Airspeed fluctuations as a measure of atmospheric turbulence
Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations
Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes
An analysis of life expectancy of airplane wings in normal cruising flight
An analysis of the skipping characteristics of some full-size flying boats
Application of a numerical procedure to stress analysis of stringer-reinforced panels
The application of data on strength under repeated stresses to the design of aircraft
Application of the method of least squares to engine-cooling analysis
Artificial running-in of piston rings
Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam rotating with constant angular velocity about a transverse axis through the root
Bending and shear stresses developed by the instantaneous arrest of the root of a moving cantilever beam
Breaking aircraft-engine oil foams by use of electrically charged condenser plates
Calculations of the Performance of a Compression-Ignition Engine-Compressor Turbine Combination I : Performance of a Highly Supercharged Compression-Ignition Engine
Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels
Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section
Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates
Charts for determining jet-boundary corrections for complete models in 7- by 10-foot closed rectangular wind tunnels
Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners
Column and plate compressive strengths of aircraft structural materials : 17S-T aluminum-alloy sheet
Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-alloy Sheet
Column and plate compressive strengths of aircraft structural materials : extruded 14S-T aluminum alloy
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