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- The effect of external shape upon the drag of a scoop
- Drag Measurements of a Protruding 0.50-Caliber Machine Gun
- Dynamic stress calculations for two airplanes in various gusts
- Determination of optimum plan forms for control surfaces
- Test of single-stage axial-flow fan
- Investigation of naphthalene as a possible aircraft fuel
- Wind-Tunnel Tests of Eight-Blade Single and Dual-Rotating Propellers in the Tractor Position
- Wind-Tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
- Wind-tunnel tests of two Hamilton Standard propellers embodying Clark Y and NACA 16 series blade sections
- A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers
- A study of the effects of vertical tail area and dihedral on the lateral maneuverability of an airplane
- Pressure distribution over an airfoil with a balanced split flap
- Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap
- Power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps
- Power-off wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane
- Wind-tunnel investigation of 20-percent-chord plain and Frise ailerons on an NACA 23012 airfoil
- Wind-tunnel investigation of an NACA 23012 airfoil with a 30 percent chord Maxwell slate and with trailing-edge flaps
- Wind-tunnel investigation of a section of the horizontal tail surface for the Bell XP-63 airplane
- Wind-tunnel investigation of an NACA 23012 airfoil with an 18.05 percent chord Maxwell slat and with trailing-edge flaps
- Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance
- Wind-tunnel investigation of control-surface characteristics II : a large aerodynamic balance of various nose shapes with a 30-percent-chord flap on an NACA 0009 airfoil
- Wind-tunnel investigation of plain ailerons for a wing with a full-span flap consisting of an inboard Fowler and an outboard retractable split flap
- Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil
- Wind-tunnel investigation of control-surface characteristics 1: effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap
- Wind-Tunnel Investigation of Perforated Split Flaps for Use as Dive Brakes on a Tapered NACA 23012 Airfoil
- Notes on the Stability and Control of Tailless Airplanes
- Annual Report of the National Advisory Committee for Aeronautics (26th). Administrative Report Including Technical Report Nos. 681 to 703
- Internal-Flow Systems for Aircraft
- A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight
- Flutter calculations in three degrees of freedom
- Determination of control-surface characteristics from NACA plain-flap and tab data
- Correction of the Lifting-Line Theory for the Effect of the Chord
- Plate method of ground representation for wind-tunnel determination of elevator effectiveness in landing
- Wind-tunnel investigation of an NACA 23012 airfoil with several arrangements of slotted flaps with extended lips
- Wind-tunnel investigation of the effect of vertical position of the wing on the side flow in the region of the vertical tail
- The Calculation of Span Load Distributions of Swept-Back Wings
- Methods of Analyzing Wind-Tunnel Data for Dynamic Flight Conditions
- The aerodynamics of a wind-tunnel fan
- The Electrical Structure of Thunderstorms
- Test of NACA 66,2-116, a =0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
- Aerodynamic Heat-Power Engine Operating on a Closed Cycle
- An investigation of the effectiveness of stiffeners on shear-resistant plate-girder webs
- An exploration of the longitudinal tensile and compressive properties throughout an extruded shape of 24S-T aluminum alloy
- Normal-pressure tests of rectangular plates
- Design of tools for press-countersinking or dimpling 0.040-inch-thick-24S-T sheet
- Rise in temperature of the charge in its passage through the inlet valve and port of an air-cooled aircraft engine cylinder
- Effect of rivet and spot-weld spacing on the strength of axially loaded sheet-stringer panels of 24S-T aluminum alloy
- Summary of results of tests made by aluminum research laboratories of spot-welded joints and structural elements
- A summary of results of various investigations of the mechanical properties of aluminum alloys at low temperatures
- The direct-stress fatigue strength of 17S-T aluminum alloy throughout the range from 1/2 to 500,000,000 cycles of stress