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- Calculated and measured turning performance of a Navy F2A-3 airplane as affected by the use of flaps
- Laminar-boundary-layer oscillations and transition on a flat plate
- De-icing of an aircraft-engine induction system
- Bearing strengths of bare and alclad XA75S-T and 24S-T81 aluminum alloy sheet
- Methods of Measurement of High Air Velocities by the Hot-Wire Method
- The effect of inlet-valve design, size, and lift on the air capacity and output of a four-stroke engine
- Flight measurements of the effect of various amounts of aileron droop on the low-speed lateral-control characteristics of an observation airplane
- The flow of a compressible fluid past a curved surface
- NACA Mach number indicator for use in high-speed tunnels
- The Measurement of Fuel-Air Ratio by Analysis for the Oxidized Exhaust Gas
- Flight tests of thermal ice-prevention equipment in the XB-24F airplane
- Icing tests of aircraft-engine induction systems
- The effect of compressibility on two-dimensional tunnel-wall interference for a symmetrical airfoil
- Ditching tests with 1/10-size model of the Army A-20A airplane I : calm-water tests in NACA tank no.2
- Determination of general relations for the behavior of turbulent boundary layers
- The problem of longitudinal stability and control at high speeds
- Laminar-boundary-layer oscillations and transition on a flat plate
- Some Investigations of the General Instability of Stiffened Metal Cylinders 7: Stiffened Metal Cylinders Subjected to Combined Bending and Torsion
- Tests of Aluminum-Alloy Stiffened-Sheet Specimens Cut From an Airplane Wing
- Torsional Elastic Properties of 18:8 Chromium-Nickel Steel as Affected by Plastic Deformation and by Heat Treatment
- Turbulent Flow Between Rotating Cylinders
- Large-Deflection Theory of Curved Sheet
- Large-Deflection Theory for End Compression of Long Rectangular Plates Rigidly Clamped Along Two Edges
- Effect of Rivet Pitch Upon the Fatigue Strength of Single-Row Riveted Joints of 0.025- to 0.025-Inch 24S-T Alclad
- Effects of Prior Fatigue-Stressing of the Impact Resistance of Chromium-Molybdenum Aircraft Steel
- Description of Stress-Strain Curves by Three Parameters
- The Stability of Isotropic or Orthotopic Cylinders or Flat or Curved Panels, Between and Across Stiffeners, With Any Edge Conditions Between Hinged and Fixed, Under Any Combination of Compression and Shear
- The Strength of Thin-Wall Cylinders of D Cross Section in Combined Pure Bending and Torsion
- Round Heat-Treated Chromium-Molybdenum-Steel Tubing Under Combined Loads
- Tensile and Compressive Tests of Magnesium Alloy J-1 Sheet
- A Theoretical Investigation of the Rolling Oscillations of an Airplane With Ailerons Free
- A Theoretical Investigation of the Lateral Oscillations of an Airplane With Free Rudder With Special Reference to the Effect of Friction
- Progress Report on Fatigue of Spot-Welded Aluminum
- Protection of Nonmetallic Aircraft From Lighting 1: General Analysis
- Protection of Nonmetallic Aircraft From Lightning 2: Lightning Conductor Materials
- The Flow of a Compressible Fluid Past a Curved Surface
- Working Charts for the Computation of Propeller Thrust Throughout the Take-Off Range
- Tests of a 1/40-Scale Wing-Hull Model and a 1/10-Scale Float-Strut Model of the Hughes-Kaiser Cargo Airplane in the Two-Dimensional Low-Turbulence Pressure Tunnel
- Tests of Airfoils Designed to Delay the Compressibility Burble
- Tests in the NACA Two-Dimensional Low-Turbulence Tunnel of Airfoil Sections Designed to Have Small Pitching Moments and High Lift-Drag Ratios
- Porpoising: A Comparison of Theory With Experiment
- Wind-Tunnel Investigation of Wing Ducts on a Single Engine Pursuit Airplane
- Methods and Charts for Computing Stability Derivatives of a V-Bottom Planing Surface
- Effect of Length-Beam Ration on Resistance and Spray of Three Models of Flying-Boat Hulls
- Investigation for the Development of a High-Speed Antiaircraft Tow Target
- Free-Flight-Tunnel Investigation of the Effect of Mode of Propeller Rotation Upon the Lateral-Stability Characteristics of a Twin-Engine Airplane Model With Single Vertical Tails of Different Size
- Flying Qualities and Stalling Characteristics of North American XP-51 Airplane
- Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model
- Construction of Wire Strain Gages for Engine Application
- Preliminary Aerodynamic and Structural Tests Showing the Effect of Compressive Load on the Fairness of a Low-Drag Wing Specimen With Chordwise Hat-Section Stiffeners