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• The application of basic data on planing surfaces to the design of flying-boat hulls
• Airfoil Theory at Supersonic Speed
• Corrugated metal diaphragms for aircraft pressure-measuring instruments
• Pressure drop in tank and float vent tubes on diving airplanes
• An approximate spin design criterion for monoplanes
• Determination of the Profile Drag of an Airplane Wing in Flight at High Reynolds Numbers
• Local Instability of Centrally Loaded Columns of Channel Section and Z-Section
• Photoelastic Analysis of Three-Dimensional Stress Systems Using Scattered Light
• Pressure-Distribution Investigation of an N.A.C.A. 0009 Airfoil With a 50-Percent-Chord Plain Flap and Three Tabs
• Propeller Tests to Determine the Effect of Number of Blades at Two Typical Solidities
• 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