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• The Design of Airplane Wing Ribs
• Elastic Instability of Members Having Sections Common in Aircraft Construction
• A Method of Calculating the Ultimate Strength of Continuous Beams
• Aircraft Woods: Their Properties, Selection, and Characteristics
• The Torsion of Members Having Sections Common in Aircraft Construction
• The Vortex Theory and Its Significance in Aviation
• Riveting in Metal Airplane Construction Part 1 : Riveting Methods and Equipment in German Metal Airplane Construction
• Velocity Distribution in the Boundary Layer of a Submerged Plate
• Les Mureaux "130.a2" Observation Airplane (French): A High-Wing Two-Seat Monoplane
• The Fiat "TR.1" Training and Touring Airplane (Italian): A Two-Place High-Wing Monoplane
• An Accurate Method of Measuring the Moments of Inertia of Airplanes
• Alterations and Tests of The "Farnboro" Engine Indicator
• Test of an Adjustable Pitch Model Propeller at Four Blade Settings
• Injection Labs in a Common-Rail Fuel Injection System
• Rate of Heat Transfer From Finned Metal Surfaces
• The Prevention of the Ice Hazard on Airplanes
• Performance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles
• Pressure distribution over a Douglas wing tip on a biplane in flight
• Strength in Shear of the Thin Curved Sheets of Alclad
• Span load distribution on two monoplanes wing models as affected by twist and sweepback
• Identification of Aircraft Tubing by Rockwell Test
• Experiments with a model water tunnel
• Effect of Orifice Length-Diameter Ratio on Spray Characteristics
• An investigation of the phenomenon of separation in the air flow around simple quadric cylinders
• An Investigation of Airplane Landing Speeds
• Methods for the Identification of Aircraft Tubing of Plain Carbon Steel and Chromium-Molybdenum Steel
• Some Characteristics of Fuel Sprays From Open Nozzles
• Analytical Determination of the Load on a Trailing Edge Flap
• Effect of the Angular Position of the Section of a Ring Cowling on the High Speed of an XF7C-1 Airplane
• A balanced diaphragm type of maximum cylinder pressure indicator
• Pressure distribution on the tail surfaces of a PW-9 pursuit airplane in flight
• Full Scale Drag Tests on Various Parts of Fairchild (FC-2W2) Cabin Monoplane
• The Structure and Properties of Parachute Cloths
• Calibration and lag of a Friez type cup anemometer
• Comparative Performance Obtained With XF7C-1 Airplane Using Several Different Engine Cowlings
• Refrigerated wind tunnel tests on surface coatings for preventing ice formation
• The Effect of Wing Tip Floating Ailerons on the Autorotation of a Monoplane Wing Model
• Some effects of air and fuel oil temperatures on spray penetration and dispersion
• The 1929 Rhon soaring-flight contest
• Bending Tests of Metal Monocoque Fuselage Construction
• The Production of Turbulence
• Relative economy of different methods of airplane construction
• The development, design and construction of gliders and sailplanes
• Estimated Effect of Ring Cowl on the Climb and Ceiling of an Airplane
• Aircraft accidents : method of analysis
• Effect of turbulence in wind-tunnel measurements
• The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level
• The Supermarine S.6.B. Racing Seaplane (British) : A Low-Wing Twin-Float Monoplane
• A proof of the theorem regarding the distribution of lift over the span for minimum induced drag
• Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials