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- Aerodynamic Characteristics of Several Airfoils of Low Aspect Ratio
- The Aerodynamic Forces and Moments on a Spinning Model of the F4B-2 Airplane as Measured by the Spinning Balance
- Analysis of a Strut With a Single Elastic Support in the Span, With Applications to the Design of Airplane Jury-Strut Systems
- Propeller vibrations and the effect of the centrifugal force
- Vortex Noise From Rotating Cylindrical Rods
- Performance tests of a single-cylinder compression-ignition engine with a displacer piston
- Strength Tests of Thin-Walled Duralumin Cylinders in Combined Transverse Shear and Bending
- Tank tests of a model of a flying-boat hull with a fluted bottom
- Full-scale force and pressure-distribution tests on a tapered U.S.A. 45 airfoil
- Bending Stresses Due to Torsion in Cantilever Box Beams
- Strength tests of thin-walled duralumin cylinders of elliptic section
- Spinning Characteristics of Wings 2: Rectangular Clark Y Biplane Cellule: 25 Percent Stagger; 0 Degree Decalage; Gap/Chord 1.0
- A general tank test of NACA model 11-C flying-boat hull, including the effect of changing the plan form of the step
- The Effect of Depth of Step on the Water Performance of a Flying-Boat Hull Model N.A.C.A. Model 11-C
- The thermodynamics of combustion in the Otto cycle engine
- A preliminary determination of normal accelerations on racing airplanes
- The Compressibility Burble
- Comparative Tests of Pitot-Static Tubes
- The Effect of the Angle of Afterbody Keel on the Water Performance of a Flying-Boat Hull Model
- The Initial Torsional Stiffness of Shells With Interior Webs
- Tank tests of a model of a flying-boat hull having a longitudinally concave planing bottom
- A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads
- Flight tests of a balanced split flap with particular reference to rapid operation
- Drag of Prestone and Oil Radiators on the YO-31A Airplane
- Development of the N.A.C.A. Slot-Lip Aileron
- The 1934 Contest for the Deutsch De La Meurthe Trophy
- Wind-tunnel tests of a wing with a trailing-edge auxiliary airfoil used as a flap
- Calculations of the Effect of Wing Twist on the Air Forces Acting on a Monoplane Wing
- Principal Effects of Axial Load on Moment-Distribution Analysis of Rigid Structures
- Status of Wing Flutter
- Considerations of the Take-Off Problem
- Tank Tests of the Effect of Rivet Heads, etc., on the Water Performance of a Seaplane Float, Special Report
- Mixture distribution in a single-row radial engine
- Impact of a vee-type seaplane on water with reference to elasticity
- Bending of beams of thin sections
- Behavior of turbulent boundary layers on curved convex walls
- Torsion and buckling of open sections
- High-speed wind tunnels
- Contribution to the problem of airfoils spanning a free jet
- General instability criterion of laminar velocity distributions
- The stress criterion of a tension member with graded flexural stiffness: contribution to the problem of "clamping effect" outside of the elastic range
- Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics
- Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel
- The measurement of the field of view from airplane cockpits
- Full-scale tests of NACA cowlings
- Air flow in the boundary layer near a plate
- Characteristics of the NACA 23012 airfoil from tests in the full-scale and variable-density tunnels
- Characteristics of six propellers including the high-speed range
- Flight investigation of lateral control devices for use with full-span flaps
- Altitude-pressure tables based on the United States standard atmosphere