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Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 2: similarity with respect to stationary polar coordinates

Wind-tunnel investigation of the damping in roll of the Bell X-1E research airplane and its components at supersonic speeds

Wind-tunnel investigation of the damping in roll of the Bell X-1A research airplane and its components at supersonic speeds

Wind-tunnel investigation of the damping in roll of the Douglas D-558-II research airplane and its components at supersonic speeds

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 1: similarity with respect to stationary rectangular coordinates

Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers

Cross flows in laminar incompressible boundary layers

Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics

Qualitative study of flow characteristics through single-stage turbines as made from rotor-exit surveys

A description of the Ames 2- by 2-foot transonic wind tunnel and preliminary evaluation of wall interference

Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane

A study of the high-speed performance characteristics of 90 degrees bends in circular ducts

A study of the efficiency of high-strength, steel, cellular-core sandwich plates in compression

Preliminary investigation of methods to increase base pressure of plug nozzles at Mach 0.9

Theoretical performance of JP-4 fuel with a 70-30 mixture of fluorine and oxygen as a rocket propellant 2: Equilibrium composition

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 1: frozen composition

Investigation of a related series of turbine-blade profiles in cascade

Summary of subsonic-diffuser data

Analysis of some parameters used in correlating blowing-type boundary-layer control data

Aerodynamic heating of aircraft components

Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0

Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces

Effect of leading-edge geometry on boundary-layer transition at Mach 3.1

Free-flight investigation of the control effectiveness of a differentially deflected horizontal tail at Mach numbers from 0.8 to 1.6

Performance of a short turbojet combustor with hydrogen fuel in a quarter-annulus duct and comparison with performance in a full-scale engine

Performance at simulated high altitudes of a prevaporizing annular turbojet combustor having low pressure loss

Investigation of the effectiveness of boundary-layer control by blowing over a combination of sliding and plain flaps in deflecting a propeller slipstream downward for vertical take-off

Preliminary investigation of the effectiveness of a sliding flap in deflecting a propeller slipstream downward for vertical take-off

Subsonic wind-tunnel investigation of the effect of fuselage afterbody on directional stability of wing-fuselage combinations at high angles of attack

Preflight and flight-test investigation of a 50-percent-magnesium 50-percent JP-4 slurry fuel in a twin engine ram-jet vehicle

Impingement of Water Droplets on a Rectangular Half Body in a Two-Dimensional Incompressible Flow Field

Relation of Turbojet Propulsion System Development to the Strategic Bomber Mission

On the Permeability of Porous Materials

Large-Scale Wind-Tunnel Tests of an Airplane Model With a 45 Degree Sweptback Wing of Aspect Ratio 2.8 With Area Suction Applied to Trailing-Edge Flaps and With Several Wing Leading-Edge Modifications

Effect of Throat Bleed on the Supersonic Performance of a Half-Conical Side-Inlet System

Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration

Perforated Sheets as a Porous Material for Distributed Suction and Injection

The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Some Linear Dynamics of Two-Spool Turbojet Engines

Stall Propagation in Axial-Flow Compressors

Space Heating Rates for Some Premixed Turbulent Propane-Air Flames

Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 10 Degrees

Generalized Tables of Corrections to Thermodynamic Properties for Nonpolar Gases

Attenuation in a Shock Tube Due to Unsteady-Boundary-Layer Action

A Theory for the Elastic Deflections of Plates Integrally Stiffened on One Side

Tabulation of the F(Sub Lambda) Functions Which Occur in the Aerodynamic Theory of Oscillating Wings in Supersonic Flow

Influence of Temperature on Creep, Stress-Rupture and Static Properties of Melamine-Resin and Silicone-Resin Glass-Fabric Laminates

Influence of Large Amplitudes on Flexural Motions of Elastic Plates

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