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• A Study of Curvilinear Flight
• Static Longitudinal Stability Of "Ente" Airplanes
• Investigation of Certain Wing Shapes With Sections Varying Progressively Along the Span
• The Dangerous Sideslip of a Stalled Airplane and Its Prevention
• The Dangerous Flat Spin and the Factors Affecting It
• Determination of Resistance and Trimming Moment of Planing Water Craft
• Elmira Soaring Contest, 1930
• Eleventh Rhön Soaring-Flight Contest, 1930
• The Use of Elektron Metal in Airplane Construction
• On Floats and Float Tests
• Clerget 100 Hp Heavy-Oil Engine
• Spatial Buckling of Various Types of Airplane Strut Systems
• Lift Distribution and Longitudinal Stability of an Airplane
• Measurements of Vertical Air Currents in the Atmosphere
• The Amiot 140 M Military Airplane (French): An All-Metal Multiplace High-Wing Monoplane
• Breguet 390 T Commercial Airplane (French): A Ten-Seat All-Steel Sesquiplane
• Breguet Military Airplane, Type 33: A Two-Place Long-Distance Sesquiplane for Observation and Bombing
• The Mono-Spar Light Airplane (British): A Twin-Engined Low-Wing Cabin Monoplane
• The Mureaux 111 R.2 Military Airplane (French): A Long-Distance All-Metal Observation Monoplane
• Polish P Type Single-Seat Fighters: All-Metal Gull-Type Wing Monoplanes
• The Dewoitine D.30 Commercial Airplane (French): A High-Wing Cantilever Monoplane
• The Dewoitine D 33 Commercial Airplane (French): A Low-Wing Cantilever Monoplane
• The Guilleman J.G. 10 (French) : A Two-Place Touring Low-Wing Monoplane
• The Mauboussin M 11 Touring Airplane (French): A Two-Place High-Wing Monoplane
• The Use of Slots for Increasing the Lift of Airplane Wings
• Mechanical Similitude and Turbulence
• Definition of Method of Measurement of Supporting and Control Surface Areas
• Airplane Landing Gear
• Method of Determining the Weights of the Most Important Simple Girders
• Wind Tunnel of the Bucharest Polytechnic Institute
• Drop and Flight Tests on NY-2 Landing Gears Including Measurements of Vertical Velocities at Landing
• Annual Report of the National Advisory Committee for Aeronautics (16th). Administrative Report Including Technical Reports Nos. 337 to 364
• The 7 by 10 Foot Wind Tunnel of the National Advisory Committee for Aeronautics
• The Design and Development of an Automatic Injection Valve With an Annular Orifice of Varying Area
• Airship Model Tests in the Variable Density Wind Tunnel
• Span-load distribution as a factor in stability in roll
• The drag characteristics of several airships determined by deceleration tests
• Tests of nacelle-propeller combinations in various positions with reference to wings. Part I : thick wing-N.A.C.A. cowled nacelle-tractor propeller
• The effect of increased carburetor pressure on engine performance at several compression ratios
• Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines
• The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines
• Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability
• A method for computing leading-edge loads
• The vertical wind tunnel of the National Advisory Committee for Aeronautics
• Focke-Wulf F 19a "Ente" Commercial Airplane (German): A Tail-First High-Wing Monoplane
• The Aerodynamic Wind Vane and the Inherent Stability of Airplanes
• Downwash Measurements Behind Wings With Detached Float
• The New "Charlestop" Remote Brake Transmission and Control
• Optico-Photographic Measurements of Airplane Deformations
• Combined Pitching and Yawing Motion of Airplanes