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- A Theoretical Study of the Dynamic Properties of Helicopter-Blade Systems
- On the Interpretation of Combined Torsion and Tension Tests of Thin-Wall Tubes
- Buckling of a Long Square Tube in Torsion and Compression
- Appreciation and Prediction of Flying Qualities
- Standard Symbols for Helicopters
- Symbols for Combustion Research
- Minimum-Weight Design of Simply Supported Transversely Stiffened Plates Under Compression
- Application of Statistical Methods to Study of Gas-Turbine Blade Failures
- Investigation of an Approximately 0.178-Chord-Thick NACA 6-Series-Type Airfoil Section Equipped With Sealed Internally Balanced 0.20-Chord Ailerons and With a 0.05-Chord Tab
- Effect of Screens in Wide-Angle Diffusers
- Effect of Rotor-Blade Twist and Plan-Form Taper on Helicopter Hovering Performance
- Flight Investigation of Effects of Rotor-Blade Twist on Helicopter Performance in the High-Speed and Vertical-Autorotative-Descent Conditions
- A Generalized Theoretical and Experimental Investigation of the Motions and Hydrodynamic Loads Experienced by V-Bottom Seaplanes During Step-Landing Impacts
- A Generalized Theoretical Investigation of the Hydrodynamic Pitching Moments Experienced by V-Bottom Seaplanes During Step-Landing Impacts and Comparisons With Experiment
- Flight Investigation of a Combined Geared Unbalancing-Tab and Servotab Control System as Used With an All-Movable Horizontal Tail
- The Experimental Determination of the Moments of Inertia of Airplanes by a Simplified Compound-Pendulum Method
- Influence of Crystal Plane and Surrounding Atmosphere on Some Types of Friction and Wear Between Metals
- The Stability Derivatives of Low-Aspect-Ratio Triangular Wings at Subsonic and Supersonic SPeeds
- Strength Tests of Shear Webs With Uprights Not Connected to the Flanges
- Wind-Tunnel Investigation of a Systematic Series of Modifications to a Flying-Boat Hull
- Wind-Tunnel Investigation of an NACA 0009 Airfoil With 0.25-and 0.50-Airfoil-Chord Plain Flaps Tested Independently and in Combination
- Theoretical and Experimental Wing-Tip Accelerations of a Small Flying Boat During Landing Impacts
- Influence of Crystal Plane and Surrounding Atmosphere on Chemical Activities of Single Crystals of Metals
- Influence of Tail Length Upon the Spin-Recovery Characteristics of a Trainer-Type-Airplane Model
- Plastic Buckling of a Rectangular Plate Under Edge Thrusts
- Dislocation Theory of the Fatigue of Metals
- Stress and Distortion Measurements in a 45 Degree Swept Box Beam Subjected to Bending and to Torsion
- Tensile, Fatigue, and Creep Properties of Forged Aluminum Alloys at Temperatures Up to 800 F
- On Similarity Rules for Transonic Flows
- Chordwise Pressure Distributions on a 12-Foot-Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60
- Mechanical Properties of Five Laminated Plastics
- High-Temperature Attack of Various Compounds on Four Heat-Resisting Alloys
- A Study of Ceramic Coatings for High-Temperature Protection of Molybdenum
- A Graphical Method for Interpolation of Specific Flying Boats From Collapsed Results of General Tests of Flying-Boat-Hull Models
- Cylinder-Head Temperatures and Coolant Heat Rejections of a Multicylinder, Liquid-Cooled Engine of 1710-Cubic-Inch Displacement
- Prediction of the Effects of Propeller Operation on the Static Longitudinal Stability of Single-Engine Tractor Monoplanes with Flaps Retracted
- Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 24S-T Sheet
- Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 24S-T81 Sheet
- Chordwise and Spanwise Loadings Measured at Low Speed on a Triangular Wing Having an Aspect Ratio of Two and an NACA 0012 Airfoil Section
- The Effect of Wind Bending Deflection on the Rolling Moment Due to Sideslip
- A Device for Measuring Sonic Velocity and Compressor Mach Number
- Method for Calculation of Pressure Distributions on Thin Conical Bodies of Arbitrary Cross Section in Supersonic Stream
- De-Icing Effectiveness of External Electric Heaters for Propeller Blades
- Characteristics of Low-Aspect Ratio Wings at Supercritical Mach Numbers
- Buckling Tests of Flat Rectangular Plates Under Combined Shear and Longitudinal Compression
- Tensile and Compressive Properties of Laminated Plastics at High and Low Temperatures
- Effect of Partial Wing Lift in Seaplane Landing Impact
- Shear Flows in Multicell Sandwich Sections
- Fracture Strength of 75S-T Aluminum Alloy Under Combined Stress
- Analytical Method of Determining Transmission of Particles and Radiation Through Great Thickness of Matter