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- NACA Investigation of a Jet-Propulsion System Applicable to Flight
- Wind Tunnel Investigation of Control Surface Characteristics: [Part] 12 - Various Cover-Plate Alinements on the NACA 0015 Airfoil With a 30 Percent Chord Flap and Large Sealed Internal Balance
- Wind-tunnel investigation of profile drag and lift of an intermediate wing section of the XP-51 airplane with beveled trailing-edge and contour ailerons
- Wind-tunnel investigation of control-surface characteristics 13: various flap overhangs used with a 30-percent-chord flap in an NACA 66-009 airfoil
- Wind-Tunnel Investigation of the Characteristics of Blunt-Nose Ailerons on a Tapered Wing
- Part-Throttle Operation and Control of a Piston-Ported Two-Stroke Cylinder
- Representative Operating Charts of Propellers Tested in the NACA 20-Foot Propeller-Research Tunnel
- Some Investigations of the General Instability of Stiffened Metal Cylinders 5: Stiffened Metal Cylinders Subjected to Pure Bending
- A Hot-Wire Circuit With Very Small Time Lag
- Principles of Moment Distribution Applied to Stability of Structures Composed of Bars or Plates
- Thermodynamic Design of Double-Panel, Air-Heated Windshields for Ice Prevention
- Emergency Measures for Increasing the Range of Fighter Airplanes
- Analysis of Wind-Tunnel Stability and Control Tests in Terms of Flying Qualities in Full-Scale Airplanes
- An Investigation of Aircraft Heaters 9: Measured and Predicted Performance of Two Exhaust Gas-Air Heat Exchangers and an Apparatus for Evaluating Exhaust Gas-Air Heat Exchangers
- The effect of altitude on cooling
- Derivation of charts for determining the horizontal tail load variation with any elevator motion
- Adaptor for Measuring Principal Strains With Tuckerman Strain Gage
- Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
- Performance of NACA eight-stage axial-flow compressor at simulated altitude
- The NACA balanced-diaphragm dynamometer-torque indicator
- Compressibility and Heating Effects on Pressure Loss and Cooling of a Baffled Cylinder Barrel
- A Concise Theoretical Method for Profile-Drag Calculation; Advance Report
- Profile-drag coefficients of conventional and low-drag airfoils as obtained in flight
- Investigation of effects of various camouflage paints and painting procedures on the drag characteristics of an NACA 65 sub (421), sup -420, A = 1.0 airfoil section
- Performance tests of wire strain gages 1: calibration factors in tension
- Nondestructive test methods for spot welds in aluminum alloys
- Effect of curvature on strength of axially loaded sheet-stringer panels
- Bibliography of piston ring lubrication
- Determination of stress-strain relations from "offset" yield strength values
- Development of detonation detector suitable for use in flight
- The shear of aluminum alloy driven rivets as affected by increasing D/t ratios
- A unit laboratory engine oil system providing for a remote indication of oil flow and oil consumption together with blow-by measurement
- An automatic electrical analyzer for 45 degree strain-rosette data
- Numerical procedures for the calculation of the stresses in Monocoques I : diffusion of tensile stringer loads in reinforced panels
- Numerical procedures for the calculation of the stresses in monocoques II : diffusion of tensiles stringer loads in reinforced flat panels with cut-outs
- Charts for rapid analysis of 45 degree strain-rosette data
- Elastic properties of channels with unflanged lightening holes
- Wind Tunnel Investigation of the Effects of Slot Shape and Flap Location on the Characteristics of a Low-Drag Airfoil Equipped with a 0.25-Chord Slotted Flap
- Wind-tunnel investigation of ailerons on a low-drag airfoil 1: The effect of aileron profile
- Wind-tunnel investigation of the effects of profile modification and tabs on the characteristics of ailerons on a low-drag airfoil
- Wind-tunnel investigation of ailerons on a low-drag airfoil 2: the effect of thickened and beveled trailing edges
- Full-scale wind-tunnel investigation of forward underslung cooling-air ducts
- High-speed aerodynamic characteristics of a four-engine bomber airplane as determined from tests of a 0.075-scale model
- High-altitude cooling VI : axial-flow fans and cooling power
- High-altitude cooling IV : intercoolers
- High-altitude cooling II : air-cooled engines
- High-altitude cooling V : cowling and ducting
- High-altitude cooling I : resume of the cooling problem
- High-speed aerodynamic characteristics of a four-engine transport airplane as determined from tests of a 0.075-scale model
- An investigation of aircraft heaters 17: experimental inquiry into steady state unidirectional heat-meter corrections