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- Thermodynamic Charts for the Computation of Combustion and Mixture Temperatures at Constant Pressure
- Effect of Ratio of Rivet Pitch to Rivet Diameter on the Fatigue Strength of Riveted Joints of 24S-T Aluminum Alloy Sheet
- Effect of the NACA Injection Impeller on the Mixture Distribution of a Double-Row Radial Aircraft Engine
- Effect of Compressibility on Section Characteristics of an Airfoil With a Round-Nose Slotted Fraise Aileron
- Development of a Protected Air Scoop for the Reduction of Induction-System Icing
- Compressive Strength of 24S-T Aluminum-Alloy Flat Panels With Longitudinal Formed Hat-Section Stiffeners
- Flight Investigation of the Effect of a Local Change in Wing Contour on Chordwise Pressure Distribution at High Speeds
- An Analysis of the Factors Affecting the State of Fuel and Air Mixtures
- The Fatigue Characteristics of Bolted Lap Joints of 24S-T Alclad Sheet Materials
- The effect of geometric dihedral on the aerodynamic characteristics of a 40 degree swept-back wing of aspect ratio 3
- Effect of brake forming on the strength of 24S-T aluminum-alloy sheet
- Flutter and oscillating air-force calculations for an airfoil in a two-dimensional supersonic flow
- Effect of change in cross section upon stress distribution in circular shell-supported frames
- Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel
- Theoretical lift and drag of thin triangular wings at supersonic speeds
- Thin oblique airfoils at supersonic speed
- Comparison of measured and calculated stresses in built-up beams
- An investigation of additional requirements for satisfactory elevator control characteristics
- Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine
- Measurements of landing-gear forces and horizontal-tail loads in landing tests of a large bomber-type airplane
- Investigation of the effect of a tip modification and thermal de-icing air flow on propeller performance
- Tank Tests to Determine the Effect of Varying Design Parameters of Planing-Tail Hulls 1: Effect of Varying Length, Width, and Plan-Form Taper of Afterbody
- The effect of simulated icing on propeller performance
- Flight tests of an all-movable horizontal tail with geared unbalancing tabs on the Curtiss XP-42 airplane
- Wing plan forms for high-speed flight
- Boundary-layer-control tests of two wings in the Langley Propeller-Research Tunnel
- Calculation of surface temperatures in steady supersonic flight
- Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections
- The effects of various parameters on the load at which spray enters the propellers of a flying boat
- Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling
- Experimental determination of the effects of dihedral, vertical-tail area, and lift coefficient on lateral stability and control characteristics
- General tank tests of a 1/10-size model of the hull of the Boeing XPBB-1 flying boat - Langley Tank Model 175
- Jet-boundary and plan-form corrections for partial-span models with reflection plane, end plate, or no end plate in a closed circular wind tunnel
- Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps
- Structural hinge-moment increments caused by hinge-axis distortion
- Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap
- Two-dimensional wind-tunnel investigation of sealed 0.22-airfoil-chord internally balanced ailerons of different contour on an NACA 65(112)- 213 airfoil
- Resume of Wind-Tunnel Data on the Effect of External Stores on Stability of Models of Military Airplanes
- An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air
- A Preliminary Investigation of the Icing Characteristics of a Large Rectangular-Throat Pressure-Type Carburetor
- An Experimental Investigation of Flow Conditions in the Vicinity of an NACA D(Sub S)-Type Cowling
- Single-Cylinder Engine Tests of Porous Chrome-Plated Cylinder Barrels With Special Bore Coatings for Radial Air-Cooled Engines
- Spray Characteristics of a Powered Dynamic Model of a Flying Boat Having a Hull With a Length-Beam Ratio of 9.0
- Stalling of Helicopter Blades
- A Preliminary Theoretical Study of Helicopter-Blade Flutter Involving Dependence Upon Coning Angle and Pitch Setting
- Wind-Tunnel Investigation of an NACA 66-Series 16-Percent-Thick Low-Drag Tapered Wing With Fowler and Split Flaps
- Tank Investigation of a Powered Dynamic Model of a Large Long-Range Flying Boat
- Two-Dimensional Wind-Tunnel Investigation of Two NACA Low-Drag Airfoil Sections Equipped With Slotted Flaps and a Plain NACA Low-Drag Airfoil Section for XF6U-L Airplane
- Static-Pressure Error of an Airspeed Installation on an Airplane in High-Speed Dives and Pullouts
- Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections