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- Some Systematic Model Experiments on the Porpoising Characteristics of Flying-Boat Hulls
- Preliminary Tests to Determine the Dynamic Stability Characteristics of Various Hydrofoil Systems for Seaplanes and Surface Boats
- Preliminary Investigation of the Effect of Compressibility on the Maximum Lift Coefficient, Special Report
- Tables of Stiffness and Carry-Over Factor for Flat Rectangular Plates Under Compression
- Shear Tests on DuPont Explosive Rivets With the Countersunk Head Milled Flush After Expansion
- The Use of a Retractable Planing Flap Instead of a Fixed Step on a Seaplane
- Proposal for a Propeller Side-Force Factor
- Relation of Preignition and Knock to Allowable Engine Temperatures
- Recommended Test Procedure for Aircraft Engine Turbosupercharger Power Plants
- Stresses Around Rectangular Cut-Outs in Skin-Stringer Panels Under Axial Loads 2
- A Study of the Effects of Radii of Gyration and Altitude on Aileron Effectiveness at High Speed
- Resume of Hinge-Moment Data for Unshielded Horn- Balanced Control Surfaces
- Some Analyses of Systematic Experiments on the Resistance and Porpoising Characteristics of Flying-Boat Hulls
- Some Notes on the Determination of the Stick-Fixed Neutral Point From Wind-Tunnel Data
- Some Systematic Model Experiments of the Bow-Spray Characteristics of Flying-Boat Hulls Operating at Low Speeds in Waves
- Some Yawing Tests of a 1/30-Scale Model of the Hull of the XPB2M-1 Flying Boat
- Theoretical Analysis of the Lateral Stability of a Glider Towed by Twin Parallel Towlines
- Use of Stagnation Temperature in Calculating Rate of Heat Transfer in Aircraft Heat Exchangers
- Wind-Tunnel Investigation of a Plain Aileron with Various Trailing-Edge Modifications on a Tapered Wing 3: Ailerons with Simple and Spring-Linked Balancing Tabs
- Wind-Tunnel Investigation of an NACA 23012 Airfoil With a 0.30-Airfoil-Chord Double Slotted Flap
- Wind-Tunnel Investigation of Control-Surface Characteristics 14: NACA 0009 Airfoil With a 20-Percent-Chord Double Plain Flap
- Vibration Surveys of the P-47-B Rudder and Fin-Rudder Assembly
- Vibration Surveys of the P-40 Rudder and Fin-Rudder Assembly
- Wind-Tunnel Investigation of a Full-Span Retractable Flap in Combination With Full-Span Plain and Internally Balanced Ailerons on a Tapered Wing
- The Measurement of Fuel-Air Ratio by Analysis of the Oxidized Exhaust Gas
- The Advantages of Uniform Fuel Distribution for Air-Cooled Engines From Considerations of Cooling Requirements and Fuel Economy
- Altitude Rating of Electrical Apparatus
- Flight Investigation of NACA D(Sub S) Cowlings on the XP-42 Airplane 1: High-Inlet-Velocity Cowling with Propeller Cuffs Tested in High-Speed Level Flight
- Antiknock Effectiveness of Xylidines in Small-Scale Engines
- Wind Tunnel Tests of Ailerons at Various Speeds 5: Pressure Distributions Over the NACA 66,2-216 and NACA 23012 Airfoils With Various Balances on 0.20-Chord Ailerons
- Wind-Tunnel Tests of a Piston-Type Control Booster on an Airfoil and Aileron Model
- Wind Tunnel Tests of Ailerons at Various Speeds 1: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil
- Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes
- Wind-Tunnel Investigation of Rear Underslung Fuselage Ducts
- Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics 5: Symmetrically Tapered Wing With a Circular Fuselage Having a Horizontal and a Vertical Tail
- Tests of 10-Inch 24S-T Aluminum-Alloy Shear Panels With 1-1/2-Inch Holes
- Tests of Inverted Spins in the NACA Free-Spinning Tunnels
- Theory of Self-Excited Mechanical Oscillations of Hinged Rotor Blades
- Theory of Mechanical Oscillations of Rotors With Two Hinged Blades
- Tests of Exhaust Propulsion Nozzles
- Tail Buffeting
- Operating Temperatures of a Sodium-Cooled Exhaust Valve as Measured by a Thermocouple
- Heat Transfer of Airfoils and Plates
- Heat Transfer Over the Circumference of a Heated Cylinder in Transverse Flow
- Experimental Investigation of a Model of a Two-Stage Turboblower
- Experimental Investigation of Impact in Landing on Water
- Experimental Investigation of Entrance-Region Heat-Transfer Coefficients
- Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane 2: Measurements of Flying Qualities with Tail Configuration Number Two
- Critical Compressive Stress for Curved Sheet Supported Along All Edges and Elastically Restrained Against Rotation Along the Unloaded Edges
- The Effect of Mass Distribution on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free-Flight Tunnel