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• The stress criterion of a tension member with graded flexural stiffness: contribution to the problem of "clamping effect" outside of the elastic range
• Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics
• Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel
• The measurement of the field of view from airplane cockpits
• Full-scale tests of NACA cowlings
• Air flow in the boundary layer near a plate
• Characteristics of the NACA 23012 airfoil from tests in the full-scale and variable-density tunnels
• Characteristics of six propellers including the high-speed range
• Flight investigation of lateral control devices for use with full-span flaps
• Altitude-pressure tables based on the United States standard atmosphere
• Cooling of airplane engines at low air speeds
• Cooling tests of a single-row radial engine with several NACA cowlings
• Wind-tunnel tests of a 10-foot-diameter gyroplane rotor
• Electrical thermometers for aircraft
• The Latecoere 521 "Lieutenant De Vaisseau Paris" commercial flying boat (French) : a two-deck six-engine semicantilever sesquiplane
• An Approximate Spin Design Criterion for Monoplanes
• The Forces and Moments on Airplane Engine Mounts
• Mechanical Properties of Aluminum-Alloy Rivets
• Effect of Several Factors on the Cooling of a Radial Engine in Flight
• Similitude in Hydrodynamic Tests Involving Planing
• Torsion and Buckling of Open Sections
• Ignition and Flame Development in the Case of Diesel Fuel Injection
• Ignition Process in Diesel Engines
• The Impact on Floats or Hulls During Landing as Affected by Bottom Width
• Flow Phenomena on Plates and Airfoils of Short Span
• Turbulent Jet Expansion
• Methods and Formulas for Calculating the Strength of Plate and Shell Constructions as Used in Airplane Design
• Investigations on the Amount of Downwash Behind Rectangular and Elliptical Wings
• The Horsepower of Aircraft Engines and Their Maximum Frontal Area
• Details of the Construction and Production of Fuel Pumps and Fuel Nozzles for the Airplane Diesel Engine
• The Cetene Scale and the Induction Period Preceding the Spontaneous Ignition of Diesel Fuels in Bombs
• The Formation of Ice on Airplanes
• Automatic Stabilization
• Charts for Checking the Stability of Compression Members in Trusses
• Automatic Stabilization
• Chief Characteristics and Advantages of Tailless Airplanes
• Interference of Wing and Fuselage From Tests of 28 Combinations in the N.A.C.A. Variable-Density Tunnel
• The Rolling Friction of Several Airplane Wheels and Tires and the Effect of Rolling Friction on Take-Off
• A Theory for Primary Failure of Straight Centrally Loaded Columns
• Pressure Distribution Over an Airfoil Section With a Flap and Tab
• Ground-Handling Forces on a 1/40-Scale Model of the U. S. Airship "Akron"
• The Forces and Moments Acting on Parts of the XN2Y-1 Airplane During Spins
• Strength of Welded Aircraft Joints
• An Analysis of Lateral Stability in Power-Off Flight With Charts for Use in Design
• Correction of Downwash in Wind Tunnels of Circular and Elliptic Sections
• The Short "Scion Senior" Commercial Airplane (British): A Four-Engine High-Wing Cantilever Monoplane
• The Short "Empire" Commercial Flying Boat (British): An All-Metal Cantilever Monoplane
• The Avro "Anson" General-Purpose Airplane (British): A Two-Engine Low-Wing Cantilever Monoplane
• The Vickers-Supermarine "Scapa" (British): A Military Flying Boat
• The reduction of aileron operating force by differential linkage