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- Further Investigation of Preheating and Postheating in Spot-Welding 0.040-Inch Alclad 24S-T
- Charts for the Minimum-Weight Design of Multiweb Wings in Bending
- Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 0-1HTA Magnesium Alloy
- Collection and Analysis of Hinge-Moment Data on Control-Surface Tabs
- A Comparison of the Lateral Motion Calculated for Tailless and Conventional Airplanes
- Compressive-Strength Comparisons of Panels Having Aluminum-Alloy Sheet and Stiffeners With Panels Having Magnesium-Alloy Sheet and Aluminum Alloy Stiffeners
- Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 2: The Effect of Angle of Sideslip and Propeller Operation
- Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 1: Effects of Compressibility in Steady Straight and Accelerated Flight
- Flight Measurements of Internal Cockpit Pressures in Several Fighter-Type Airplanes
- The Local Buckling Strength of Lipped Z-Columns With Small Lip Width
- Application of the Analogy Between Water Flow With a Free Surface and Two-Dimensional Compressible Gas Flow
- The One-Dimensional Theory of Steady Compressible Fluid Flow in Ducts With Friction and Heat Addition
- High-Speed Wind-Tunnel Tests of an NACA 16-009 Airfoil Having a 32.9-Percent-Chord Flap With an Overhang 20.7 Percent of the Flap Chord
- An Investigation of a Thermal Ice-Prevention System for a Cargo Airplane 8: Metallurgical Examination of the Wing Leading-Edge Structure After 225 Hours of Flight Operation of the Thermal System
- Effect of Variables in Welding Technique on the Strength of Direct-Current Metal-Arc-Welded Joints in Aircraft Steel 1 - Static Tension and Bending Fatigue Tests of Joints in SAE 4130 Steel Sheet
- Free-Falls and Parachute Descents in the Standard Atmosphere
- Hinge-moment characteristics of balanced elevator and rudder for a specific tail configuration on a fuselage in spinning attitudes
- Full-scale investigation of the aerodynamic characteristics of a typical single-rotor helicopter in forward flight
- Effect of brake forming in various tempers on the strength of Alclad 75S-T aluminum-alloy sheet
- Effect of blade stalling on the efficiency of a helicopter rotor as measured in flight
- Comparison of sound emission from two-blade, four-blade, and seven-blade propellers
- Comparison of the control-force characteristics of two types of lateral-control system for large airplanes
- Design charts for flat compression panels having longitudinal extruded Y-section stiffeners and comparison with panels having formed Z-section stiffeners
- Estimation of control forces of spring-tab ailerons from wind-tunnel data
- Effect of spoiler-type lateral-control devices on the twisting moments of NACA 230-Series airfoil sections
- Effect of the tunnel-wall boundary layer on test results of a wing protruding from a tunnel wall
- Tests of the NACA 64(SUB 1)A212 airfoil section with a slat, a double slotted flap, and boundary-layer control by suction
- A transonic propeller of triangular plan form
- Tests to determine the effect of heat on the pressure drop through radiator tubes
- Theoretical motions of hydrofoil systems
- Tank investigation of a powered dynamic model of a large long-range flying boat - Langley tank model 180
- Summary of lateral-control research
- Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab
- Theoretical and experimental data for a number of NACA 6A-series airfoil sections
- Theory of ground vibrations of a two-blade helicopter rotor on anisotropic flexible supports
- Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having a ratio of stiffener thickness to skin thickness equal to 1.00
- Comparison between the measured and theoretical span loadings on a moderately swept-forward and a moderately swept-back semispan wing
- Comparison of design specifications with the actual static transverse stability of 25 seaplanes
- Charts for determining the characteristics of sharp-nose airfoils in two-dimensional flow at supersonic speeds
- Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates
- A comparison of flight test results on a scout-bomber airplane with 4.7 degree and with 10 degree geometric dihedral in the wing outer panels
- Investigation at low speed of the longitudinal stability characteristics of a 60 degree swept-back tapered low-drag wing
- Investigation of a Spoiler-Type Lateral Control System on a Wing with Full-Span Flaps in the Langley 19-Foot Pressure Tunnel
- An investigation of effects of reversed-type longitudinal steps on resistance and spray characteristics of a flying-boat hull
- Low-speed tests of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers
- Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and Alclad 75S-T sheet in incomplete diagonal tension
- Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8, 10, and 12 and taper ratios of 2.5 and 3.5
- Calculations of the supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio : wings swept behind the Mach lines
- A flight investigation to increase the safety of a light airplane
- Flight tests of an airplane model with 42 degree swetpback wing in the Langley free-flight tunnel