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• Flight Tests of Retractable Ailerons on a Highly Tapered Wing
• A Method of Estimating the Critical Buckling Load for Structural Members
• Combined Beam-Column Stresses of Aluminum-Alloy Channel Sections
• Wind-Tunnel Investigation of an N.A.C.A. 23021 Airfoil With Two Arrangements of a 40-Percent-Chord Slotted Flap
• Pressure-Distribution Measurements on a Rectangular Wing With a Partial-Span Split Flap in Curved Flight
• Tidewater and Weather-Exposure Tests on Metals Used in Aircraft
• A Recurrence Formula for Shear-Lag Problems
• Flight Tests of N.A.C.A. Nose-Slot Cowlings on the BFC-1 Airplane
• The Effects of Surface Waviness and of Rib Stitching on Wing Drag
• Wind-Tunnel Investigation of Effect of Yawing on Lateral-Stability Characteristics 2: Rectangular N.A.C.A. 23012 Wing with a Circular Fuselage and a Fin
• Measurements of the Air-Flow Velocity in the Cylinder of an Airplane Engine
• Investigations and Experiments in the Guidonia Wind Tunnel
• Investigations and Tests in the Towing Basin at Guidonia
• Measurement of the True Dynamic and Static Pressures in Flight
• Report on Ice Formation on Aircraft
• Ice Formation on Wings
• Experimental and Analytical Investigation of a Monocoque Wing Model Loaded in Bending
• Effect of Transition in Cross-Sectional Shape on the Development of the Velocity and Pressure Distribution of Turbulent Flow in Pipes
• The Breda Wind Tunnel
• The Way to Increased Airplane Engine Power
• The Power of Aircraft Engines at Altitude
• Modern Methods of Testing
• The Limit of Stability of a Curved Plate Strip Under Shear and Axial Stresses
• Investigation of the Lift Distribution Over the Separate Wings of a Biplane
• Dynamic Stability of a Helicopter With Hinged Rotor Blades
• Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil
• The Hydrodynamic Theory of Detonation
• The Enlarged N.A.C.A. Tank, and Some of Its Work
• The Effect of Streamlining the Aterbody of an N.A.C.A. Cowling
• Engine Knock and Combustion Chamber Form
• Forces and Moments on a Yawed Airfoil
• Contribution to the Aerodynamics of Rotating-Wing Aircraft
• Theory of Two-Dimensional Potential Flow About Arbitrary Wing Sections
• The Theory of Contra-Vanes Applied to the Propeller
• Theoretical and Experimental Study of Ignition Lag and Engine Knock
• Stability of Rectangular Plates With Longitudinal or Transverse Stiffeners Under Uniform Compression
• Contribution to the Theory of the Heated Duct Radiator
• Knocking in the Otto-Cycle Engine
• Meteorological-Physical Limitations of Icing in the Atmosphere
• The Effect of the Masses of the Controls on the Longitudinal Stability With Free Elevator Part 1
• Temperature-Indicating Paints
• Comparison of Theory With Experiment in the Phenomenon of Wing Flutter
• Measurements on a Low-Wing Model in the Rotating Jet and Comparison With Flight Measurements
• A Theoretical Study of the Moment on a Body in a Compressible Fluid
• Flame Speeds and Energy Considerations for Explosions in a Spherical Bomb
• Effective Gust Structure at Low Altitudes as Determined From the Reactions of an Airplane
• Determination of the Profile Drag of an Airplane Wing in Flight at High Reynolds Numbers
• Effect of Service Stress on Impact Resistance, X-Ray Diffraction Patterns, and Microstructure of 25S Aluminum Alloy
• Correlation of Cooling Data From an Air-Cooled Cylinder and Several Multicylinder Engines
• Tests of NACA 0009, 0012, and 0018 Airfoils in the Full-Scale Tunnel