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- Determination of the damping moment in yawing for tapered wings with partial-span flaps
- Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress
- Data on buckling strength of curved sheet in compression
- Tests of two models representing intermediate inboard and outboard wing sections of the XB-36 airplane
- Tests of a dynamic model in NACA tank number 1 to determine the effect of length of afterbody, angle of afterbody keel, gross load, and a pointed step on landing and planning stability
- Tank Tests of a 1/8-Size Dynamic Model of the PB2Y-3 Airplane with Simulated Jet Motors: NACA Models 131J, 131J-1 and 131J-2
- Theory and preliminary flight tests of an all-movable vertical tail surface
- Time-velocity-altitude relations for an airplane diving in a standard atmosphere
- Tank tests of a 1/8-size dynamic model of the PB2Y-3 airplane with increased power: NACA model 131
- Characteristics of an NACA 66, S-209 section hydrofoil at several depths
- Limitations of lifting-line theory for estimation of aileron hinge-moment characteristics
- Investigation of surface irregularities on an NACA 63(420)-416, a=1.0 airfoil section for the Glenn L. Martin Company design 195
- The effect of mass distribution on the lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel
- Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil
- Wind-tunnel tests of four full-scale seaplane floats
- Wind-Tunnel Tests of the 1/9-Scale Model of the Curtiss XP-62 Airplane with Various Vertical Tail Arrangements
- Wind-tunnel tests of two tapered wings with straight leading edges and with constant-chord center sections of different spans
- Wind-tunnel vibration tests of dual-rotating propellers
- Wind-tunnel tests of single and dual-rotating tractor propellers at low blade angles and of two-and three-blade tractor propellers at blade angles up to 65 degrees
- Wind-tunnel vibration tests of a four-blade single rotating pusher propeller
- Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section
- A comparison at high speed of the aerodynamic merits of models of medium bombers having thickened wing roots and having wings with nacelles
- Flight investigation of NACA D(sub S) cowlings on the XP-42 airplane 2: low-inlet-velocity cowling with axial-flow fan and propeller cuffs
- Flight investigation of NACA D(sub S) cowlings on the XP-42 airplane 4: high-inlet-velocity cowling tested in climb with and without propeller cuffs and in high-speed level flight without propeller cuffs
- Flight investigation of NACA D(sub S) cowlings on the XP-42 airplane 3: low-inlet-velocity cowling without fan or propeller cuffs, with axial-flow fan alone, and with two different sets of propeller cuffs
- Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel
- Hydrodynamic-stability tests of a model of a flying boat and of a planing surface having a small downward projection (hook) on the planing bottom near the step
- Improved baffle designs for air-cooled engine cylinders
- An experimental survey of flow across banks of elliptical and pointed tubes
- General free to trim tests in NACA tank no.2 of three 1/8-full-size models of flying-boat hulls at low speeds-NACA models 116E-3K, 120R, and 143
- Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines 1: capacity and economy
- Pressure distribution measurements on various surfaces of a 0.2375-scale model of the Douglas XA-26 airplane in the 19-foot pressure tunnel
- A preliminary study of the effect of compressive load on the fairness of a low-drag wing specimen with Z-section stiffeners
- Wind-tunnel data on the aerodynamic characteristics of airplane control surfaces
- Wind-tunnel investigation of a plain aileron with thickened and beveled trailing edges on a tapered low-drag wing
- Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap
- On a function-theory method for obtaining potential-flow patterns of a compressible fluid
- On the plane potential flow past a lattice of arbitrary airfoils
- Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
- 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