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- Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degree, 42 degree and 62 degree sweepback
- Flight tests of an airplane model with a 62 degree swept-back wing in the Langley free-flight tunnel
- Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-Series Airfoil Sections
- Boundary-Induced Upwash for Yawed and Swept-Back Wings in Closed Circular Wind Tunnels
- The streamline pattern in the vicinity of an oblique airfoil
- Stresses around rectangular cut-outs with reinforced coaming stringers
- Summary of drag characteristics of practical-construction wing sections
- Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests
- Performance of axial-flow fan and compressor blades designed for high loadings
- Low-speed stability and damping-in-roll characteristics of some highly swept wings
- Preliminary investigation at low speed of downwash characteristics of small-scale sweptback wings
- Performance of an axial-flow compressor rotor designed for a pitch-section lift coefficient of 1.20
- Notes on the theoretical characteristics of two-dimensional supersonic airfoils
- Numerical evaluation of mass-flow coefficient and associated parameters from wake-survey equations
- Charts for the Determination of Supersonic Air Flow Against Inclined Planes and Axially Symmetric Cones
- An Analysis of the Compressive Strength of Honeycomb Cores for Sandwich Construction
- Wind-tunnel investigation of the effects of surface-covering distortion on the characteristics of a flap having undistorted contour maintained for various distances ahead of the trailing edge
- Wind-tunnel investigation of unshielded horn balances on a horizontal tail surface
- Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wing
- Wind-tunnel investigation of the NACA 654-421 airfoil section with a double slotted flap and boundary layer control by suction
- Wind-tunnel investigation of the effect of wing-tip fuel tanks on characteristics of unswept wings in steady roll
- Icing Properties of Noncyclonic Winter Stratus Clouds
- Static and Dynamic Creep Properties of Laminated Plastics for Various Types of Stress
- Precautions for Flight Testing Near the Speed of Sound
- Performance Investigation of a Jumo 004 Combustor
- Preliminary Tests at Supersonic Speeds of Triangular and Swept-Back Wings
- Factors Affecting the Design of Quiet Propellers
- Experimental Investigation of a Preloaded Spring-Tab Flutter Model
- A Preliminary Theoretical Study of Aerodynamic Instability of a Two-Blade Helicopter Rotor
- Preliminary Results of a Flight Investigation to Determine the Effect of Negative Flap Deflection on High-Speed Longitudinal-Control Characteristics
- Preliminary Investigation of Two Full-Scale Propellers to Determine the Effect of Swept-Back Blade Tips on Propeller Aerodynamic Characteristics
- Preliminary Tank Tests of NACA Hydro-Skis for High-Speed Airplanes
- A Torsional Stiffness Criterion for Preventing Flutter of Wings of Supersonic Missiles
- Supersonic-Tunnel Tests of Two Supersonic Airplane Model Configurations
- Wind-Tunnel Investigation of Air Loads Over a Double Slotted Flap on the NACA 65(216)-215, a = 0.8 Airfoil Section
- Yaw Characteristics and Sidewash Angles of a 42 Degree Sweptback Circular-Arc Wing With a Fuselage and With Leading-Edge and Split Flaps at a Reynolds Number of 5,300,000
- Wind-Tunnel Investigation of Wing Inlets for a Four-Engine Airplane
- Effects of a Fuselage and Various High-Lift and Stall-Control Flaps on Aerodynamic Characteristics in Pitch of an NACA 64-Series 40 Degree Swept-Back Wing
- Effect of Number of Fins on the Drag of a Pointed Body of Revolution at Low Supersonic Velocities
- The Effect of Sample Size on the Determination of Maximum Gust Velocities in Clouds
- Effects of Combinations of Aspect Ratio and Sweepback at High Subsonic Mach Numbers
- Effects of Compressibility on the Characteristics of Five Airfoils
- Drag Measurements of a Swept-Back Wing Having Inverse Taper as Determined by Flight Tests at Supersonic Speeds
- Effect of Chordwise Vanes on Amplitude of Tail Buffeting
- Determination of Coupled Modes and Frequencies of Swept Wings by Use of Power Series
- Drag Measurements of Symmetrical Circular-Arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
- Drag Measurements of a 34 Degree Swept-Forward and Swept-Back NACA 65-009 Airfoil of Aspect Ratio 2.7 as Determined by Flight Tests at Supersonic Speeds
- Drag of a Wing-Body Configuration Consisting of a Swept-Forward Tapered Wing Mounted on a Body of Fineness Ratio 12 Measured During Free Fall at Transonic Speeds
- Air-Flow Behavior Over the Wing of an XP-51 Airplane as Indicated by Wing-Surface Tufts at Subcritical and Supercritical Speeds
- Aerodynamic Characteristics of a 42 Degree Swept-Back Wing With Aspect Ratio 4 and NACA 64(Sub 1)-112 Airfoil Sections at Reynolds Numbers From 1,700,000 to 9,500,000