Search U.S. government technical reports digitized or harvested by TRAIL.
Graphic Method for Calculating the Speed and Climbing Ability of Airplanes
Notes on Aerodynamic Forces on Airship Hulls
Experiments With a Built-In or Fuselage Radiator
Determination of the Value of Wood for Structural Purposes
Influence of Ribs on Strength of Spars
Standardization and Aerodynamics
Is There Any Available Source of Heat Energy Lighter Than Gasoline?
Experiments With Fabrics for Covering Airplane Wings
The Increase in Dimensions of Airplanes - Weight, Area, and Loading of Wings
Measuring an Airplane's True Speed in Flight Testing
Disturbing Effect of Free Hydrogen on Fuel Combustion in Internal Combustion Engines
Model Supports and Their Effects on the Results of Wind Tunnel Tests
Variation in the Number of Revolutions of Air Propellers
Thrust and Power Required in Climbing
Tests on Built-Up Airplane Struts Having Initial Tension in Outside Fibers
Notes on the N.A.C.A. Control Force Recorder
The Air Propeller, Its Strength and Correct Shape
Air Resistance Measurements on Actual Airplane Parts
Absolute Dimensions of Karman Vortex Motion
The Nichols Wing Cutting Equipment
Reduction in Efficiency of Propellers Due to Slipstream
Compressive Strength of Tapered Airplane Struts
Notes on the design of ailerons
Calculations for a Single-Strut Biplane With Reference to the Tensions in the Wing Bracing
The Fairing of Airfoil Contours
The flexible mounting of an airplane engine
Adaptation of aeronautical engines to high altitude flying
Compressive Strength of Tapered Airplane Struts
Experimental Research on Air Propellers, 5
Aeronautic instruments. Section 5 : power plant instruments
The Altitude Effect on Air Speed Indicators - 2
Tests on Air Propellers in Yaw
Mathematical Equations for Heat Conduction in the Fins of Air-Cooled Engines
Rules and Regulations of the 1922 Rhoen Soaring Flight Contest
Methods of experimentation with models and utilization of results
Calculation of the hull and of the car-suspension systems of airships
Engine performance and the determination of absolute ceiling
Analysis of W. F. Durand's and E. P. Lesley's propeller tests