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• Wind tunnel research comparing lateral control devices, particularly at high angles of attack 11: various floating tip ailerons on both rectangular and tapered wings
• Full-Scale Wind-Tunnel Research on Tail Buffeting and Wing-Fuselage Interference of a Low-Wing Monoplane
• Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage
• The Effect of Rivet Heads on the Characteristics of a 6 by 36 Foot Clark Y Metal Airfoil
• The effect of spray strips on a model of the P3M-1 flying boat hull
• Some Characteristics of Sprays Obtained from Pintle-Type Injection Nozzles
• Engine performance with a hydrogenated safety fuel
• Simplified aerodynamic analysis of the cyclogiro rotating wing system
• Charts for determining the pitching moment of tapered wings with sweepback and twist
• The 1933 Contest for the Deutsch De La Meurthe Trophy
• A Complete Tank Test of a Model of a Flying-Boat Hull - N.A.C.A. Model No.11
• Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes
• The importance of auto-ignition lag in knocking
• Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot
• Experiments with planing surfaces
• Analysis of spinning in a monoplane wing by the induction method as compared with the strip method
• The behavior under shearing stress of duralumin strip with round, flanged holes
• Aerodynamic principles of the direct lifting propeller
• The Aachen wind-tunnel balance
• Heat transfer from finned metal cylinders in an air stream
• The aerodynamic effects of wing cut-outs
• Air flow in a separating laminar boundary layer
• The estimation of maximum load capacity of seaplanes and flying boats
• Static thrust of airplane propellers
• Relative loading on biplane wings
• Tests of 16 related airfoils at high speed
• Tests of nacelle-propeller combinations in various positions with reference to wings 4: thick wing - various radial-engine cowlings - tandem propellers
• Air conditions close to the ground and the effect on airplane landings
• A flight investigation of the lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral
• The calculation of take-off run
• Experimental investigation of the Robinson-type cup anemometer
• The high-speed tank of the Hamburg Shipbuilding Company
• The Bernard 82 military airplane (French) : a long-range monoplane
• The Small Wind Tunnel of the DVL
• Impact Buckling of Thin Bars in the Elastic Range Hinged at Both Ends
• Investigation of a Rateau Supercharger for a 700-Horsepower Airplane Engine
• The Processes in Spring-Loaded Injection Valves of Solid Injection Oil Engines
• The Effect of Weight and Drag on the Sinking Speed and Lift/Drag Ratio of Gliders
• Evaluation of Scavenging in Two-Stroke-Cycle Engines
• High-Speed Aircraft
• The High-Speed Heinkel HE 70 Mail Airplane
• The Calculation of Lateral Stability With Free Controls
• Supplemental Data and Calculations of the Lateral Stability of Airplanes
• Impact Buckling of Thin Bars in the Elastic Range for Any End Condition
• Fatigue Strength of Airplane and Engine Materials
• The Development of Floats and Equipment for Research in Promoting It
• Technical Aspects of the 1934 International Touring Competition (Rundflug)
• Influence of Cut-Outs in Elevator on the Static Longitudinal Stability and on the Static Elevator Effect
• Safety and Design in Airplane Construction
• Stipa Monoplane With Venturi Fuselage