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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


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