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- An Investigation of 0.15-Chord Ailerons on a Low-Drag Tapered Wing at High Speeds
- Integral Methods in the Theory of the Boundary Layer
- High-speed investigation of low-drag wing inlets
- Scale and Turbulence Effects on the Lift and Drag Characteristics of the NACA 65(Sub 3)-418, A=1.0 Airfoil Section
- The relation between spanwise variations in the critical Mach number and spanwise load distributions
- Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap
- Resistance Tests of a 1/16 Size Model of the Hughes-Kaiser Flying Boat, NACA Model 183
- Secondary Stresses in Open Box Beams Subjected to Torsion
- The effect of cooling-air blowers on thrust power
- Flutter tests of B-34 fin-rudder-tab system
- Ditching tests with a 1/11-size model of the Army B-25 airplane in NACA tank number 2 and on an outdoor catapult
- Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company
- Comparison of an approximate and an exact method of shear-lag analysis
- A comparison of three spinner-diffuser designs in an NACA D(sub S) cowling for the Pratt & Whitney R-2800 engine
- Determination of desirable lengths of Z- and channel-section columns for local-instability tests
- Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation
- The determination of effective column length from strain measurements
- Effects of trailing-edge modifications on pitching moment characteristics of airfoils
- Ditching tests with a 1/10-size model of the Army A-20A airplane in Langley tank no.2 and on an outdoor catapult
- Correlation of flight data on limit pressure coefficients and their relation to high-speed burbling and critical tail loads
- Cooling Characteristics of a Pratt and Whitney R-2800 Engine Installed in an NACA Short-Nose High-Inlet-Velocity Cowling
- Tests of a 0.30-scale semispan model of the Douglas XTB2D-1 airplane wing and fuselage combination in the NACA 19-foot pressure tunnel 2: roll-flap positioning and lateral-control investigation
- Summary of measurements in Langley full-scale tunnel of maximum lift coefficients and stalling characteristics of airplanes
- Tensile Tests of NACA and Conventional Machine-Countersunk Flush Rivets
- Tests of a 0.30 scale semispan model of the Douglas XTB2D-1 airplane wing and fuselage combination in the NACA 19-foot pressure tunnel 1: full-span flap and air-brake investigation
- Tests of the NACA 653-018 airfoil section with boundary-layer control by suction
- Comparison of the compressive strength of panels with Alclad 24S-T81 sheet or with Alclad 24S-T86 sheet riveted to Alclad 24S-T84 hat-section stiffeners
- Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal Speed
- Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers
- Considerations of wake-excited vibratory stress in a pusher propeller
- Investigation of effects of various camouflage paints and painting procedures on the drag characteristics of an NACA 65(sub 421)-420, a = 1.0 airfoil section
- Effect of power on the stick-fixed neutral points of several single-engine monoplanes as determined in flight
- Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers
- Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons
- Wind-tunnel tests of the 1/8-scale powered model of the Curtiss XBTC-2 airplane 2: preliminary investigation of lateral stability and control
- Effect of Helicopter Performance of Modifications in Profile-Drag Characteristics of Rotor-Blade Airfoil Sections
- Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers
- Charts for estimation of the characteristics of a helicopter rotor in forward flight I: profile drag-lift ratio for untwisted rectangular blades
- Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed
- Flight investigation of boundary-layer control by suction slots on an NACA 35-215 low-drag airfoil at high Reynolds numbers
- Experimental Verification of the Rudder-Free Stability Theory for an Airplane Model Equipped with Rudders Having Negative Floating Tendency and Negligible Friction
- Effects of propeller operation and angle of yaw on the distribution of the load on the horizontal tail surface of a typical pursuit airplane
- Experimental constriction effects in high-speed wind tunnels
- The Effect of Piston-Head Temperature on Knock-Limited Power
- A Theoretical Investigation of the Rolling Oscillations of an Airplane with Ailerons Free
- Bending and Shear Stresses Developed by the Instantaneous Arrest of the Root of a Moving Cantilever Beam
- Investigation of the NACA 4-(3)(8)-045 Two-Blade Propellers at Forward Mach Numbers to 0.725 to Determine the Effects of Compressibility and Solidity on Performance
- Static-thrust and torque characteristics of single and dual rotating tractor propellers
- A proposed method of measuring engine charge air flow in flight
- A study of the effect of aftercooling on the power and the weight of a 2000-horsepower air-cooled engine installation