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- A preliminary investigation of exhaust-gas ejectors for ground cooling
- Lateral-control characteristics of North American XP-51 airplane (A. C. No. 41-38) with beveled trailing-edge ailerons in high-speed flight
- A mass-distribution criterion for predicting the effect of control manipulation on the recovery from a spin
- The Porpoising Characteristics of a Planing Surface Representing the Forebody of a Flying-Boat Hull
- Power-on longitudinal-stability and control tests of the 1/8-scale model of the Brewster F2A airplane equipped with full-span slotted flaps and a new horizontal tail
- Preliminary Investigation in the NACA Low-Turbulence Tunnel of Low-Drag Airfoil Sections Suitable for Admitting Air at the Leading Edge
- The effect of pitch on force and moment characteristics of full-scale propellers of five solidities
- The effect of spanwise mass distribution upon the spin characteristics of airplanes as determined by model tests conducted in the free-spinning wind tunnel
- Wind-tunnel investigation of a tapered wing with a plug-type spoiler-slot aileron and full-span slotted flaps
- Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing 2: ailerons with thickened and beveled trailing edges
- Methods used in the NACA tank for the investigation of the longitudinal-stability characteristics of models of flying boats
- Wind-tunnel investigation of a plain aileron and a balanced aileron on a tapered wing with full-span duplex flaps
- Multiengine airplane spin characteristics as indicated by model tests in the free-spinning wind tunnel
- Wind-Tunnel Investigation of Control-Surface Characteristics: [Part] 7 - A Medium Aerodynamic Balance of Two Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0015 Airfoil
- Wind Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics: [Part] 4 - Symmetrically Tapered Wing With a Circular Fuselage Having a Wedge-Shaped Rear and a Vertical Tail
- Wind tunnel investigation of control surface characteristics 9: some analytical considerations and experimental test results for an internally balanced flap
- Wind-tunnel investigation of control-surface characteristics 6: a 30-percent-chord plain flap on the NACA 0015 airfoil
- Wind tunnel investigation of control-surface characteristics 10: a 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil
- The Photoviscous Properties of Fluids
- Annual Report of the National Advisory Committee for Aeronautics (27th). Administrative Report Including Technical Report Nos. 704 to 726
- Flight Tests of Modifications to Improve the Aileron Control Characteristics of a North American XP-51 Airplane (AC No. 41-38)
- Column Strength of Magnesium Alloy AM-57S
- Propellers in yaw
- Wind tunnel investigation of control surface characteristics.12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance
- Bearing tests of magnesium-alloy sheet
- Torsion tests of 24S-T aluminum-alloy noncircular bar and tubing
- Torsional strength of aluminum-alloy round tubing
- Bearing strengths of some wrought-aluminum alloys
- Effect of fillers and of mixing procedure on the strength of plastic materials
- Certain mechanical strength properties of aluminum alloys 25S-T and X76S-T
- Torsion of flanged members with cross sections restrained against warping
- A portable calibrator for dynamic strain gages
- The effect of the type of specimen on the shear strengths of driven rivets
- Tests of flat panels with four types of stiffeners
- Flight measurements of the effects of a wing leading-edge slot and other modifications on the stability, maximum lift, and high speed of an observation airplane
- An investigation of aircraft heaters X : measured and predicted performance of a fluted-type exhaust gas and air heat exchanger
- An investigation of aircraft heaters VIII : a simplified method for the calculation of the unit thermal conductance over wings
- An instrument for the determination of rain densities in flight
- Investigation of methods of reducing the temperature variation among cylinders on air-cooled aircraft engines
- Measurements of friction coefficients in a pipe for subsonic and supersonic flow of air
- Method of calculating performance of dual-rotating propellers from airfoil characteristics
- A method for making quantitative studies of the main spray characteristics of flying-boat hull models
- Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
- Preliminary tank tests with planing-tail seaplane hulls
- A procedure for the shear-lag analysis of box beams
- The problem of longitudinal stability and control at high speeds
- Preliminary vibration and flutter studies on P-47 tail
- Lead susceptibility of paraffins, cycloparaffins, and olefins
- Lift and drag data for 30 pusher-propeller shaft housings on an NACA 65,3-018 airfoil section
- The locus of possible positions of a heavy bomber in space after a 12-second time interval