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• The Variation in Pressures in the Cockpit Fan Airplane in Flight
• The Reaction on a Float Bottom When Making Contact With Water at High Speeds
• The Drag of a J-5 Radial Air-Cooled Engine
• Preliminary biplane tests in the variable density wind tunnel
• A Dangerous Seaplane Landing Condition
• The Effect of the Sperry Messenger Fuselage on the Air Flow at the Propeller Plane
• Determination of Propeller Deflection by Means of Static Load Tests on Models
• Helium Tables
• Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight Part 2: pull-ups
• Drag of exposed fittings and surface irregularities on airplane fuselages
• Resistance of streamline wires
• A Comparison of Propeller and Centrifugal Fans for Circulating the Air in a Wind Tunnel
• An automatic speed control for wind tunnels
• The 1926 German Seaplane Contest
• Force Measurements on Airplanes
• An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings
• An investigation of the use of discharge valves and an intake control for improving the performance of N.A.C.A. Roots type supercharger
• Impact waves and detonation. Part II
• The comparative performance of Roots type aircraft engine superchargers as affected by change in impeller speed and displacement
• The Analysis of Aircraft Structures as Space Frameworks. Method Based on the Forces in the Longitudinal Members
• Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch
• Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane
• Aerodynamic theory and tests of strut forms. Part II
• Theories of flow similitude
• Forces on elliptic cylinders in uniform air stream
• Reduction of observed airplane performance to standard conditions
• The variation in engine power with altitude determined from measurements in flight with a hub dynamometer
• Investigation of damping liquids for aircraft instruments
• Fire prevention on airplanes. Part I
• Fire prevention on airplanes. Part II
• Airplane drag
• Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics
• Technical report of the 1928 Rhon soaring-flight contest
• Nieuport-Delage 640 (French) : commercial high-wing monoplane
• The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine
• The Blackburn "Bluebird" Mark IV (British) all-metal biplane
• The Bernard 20 C.1 (French) : a single-seat pursuit monoplane
• Torsional Rigidity of Cantilever Wings With Constant Spar and Rib Sections
• Impact Waves and Detonation: Part 1
• Landing and Braking of Airplanes
• Remarks on Airplane Struts and Girders Under Compressive and Bending Stresses: Index Values
• On the Strength of Box Type Fuselages
• The Effect of Reduction Gearing on Propeller-Body Interference as Shown by Full-Scale Wind-Tunnel Tests
• Effect of Oxygen on the Ignition of Liquid Fuels
• Experiments With a Wing Model From Which the Boundary Is Removed by Suction
• Full-Scale Wind-Tunnel Tests on Several Metal Propellers Having Different Blade Forms
• Full-Scale Wind-Tunnel Tests With a Series of Propellers of Different Diameters on a Single Fuselage
• The Gaseous Explosive Reaction at Constant Pressure: The Reaction Order and Reaction Rate
• Working Charts for the Selection of Aluminum Alloy Propellers of a Standard Form to Operate With Various Aircraft Engines and Bodies
• Welding of Stainless Materials