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NACA Research Memorandums
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Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 2: Rotor Blades With 15 Fins in Cooling-Air Passages
Interpretation of boundary-layer pressure-rake data in flow with a detached shock
Experimental and Analytical Study of Balanced-Diaphragm Fuel Distributors for Gas-Turbine Engines
Pressure Measurements on a Sharply Converging Fuselage Afterbody With Jet on and Off at Mach Numbers From 0.8 to 1.6
Effects of Varying the Size and Location of Trailing-Edge Flap-Type Controls on the Aerodynamic Characteristics of a Unswept Wing at a Mach Number of 1.9
Effect of Retractable Ignition Plug on Plug Fouling by Carbon Deposits
The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
Altitude-Test-Chamber Investigation of Performance of a 28-Inch Ram-Jet Engine 1: Combustion and Operational Performance of Four Combustion-Chamber Configurations
Effect of compressor-outlet bleedoff on turbojet-engine performance
Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 3: Methods for Determining Power and Efficiency
Determination by the Free-Fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds
Preliminary analysis of effects of air cooling turbine blades on turbojet-engine performance
Influence of tube-entrance configuration on average heat-transfer coefficients and friction factors for air flowing in an Inconel tube
The Effect of Changes in the Leading-Edge Radius on the Aerodynamic Characteristics of a Symmetrical, 9-Percent-Thick Airfoil at High-Subsonic Mach Numbers
Investigation at High Subsonic Speeds of Methods of Alleviating the Adverse Interference at the Root of a Swept-Back Wing
Altitude performance characteristics of tail-pipe burner with variable-area exhaust nozzle
Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of the Buffet Boundary and Peak Airplane Normal-Force Coefficients at Mach Numbers Up to 0.90
Extension of boundary-layer heat-transfer theory to cooled turbine blades
Altitude-wind-tunnel investigation of operational characteristics of J47 turbojet engine
Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section: Transonic-bump method
Wing-flow measurements of longitudinal stability and control characteristics of a canard airplane configuration with a 45 degree sweptback wing and a triangular all-movable control surface
Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
Penetration of Liquid Jets into a High-Velocity Air Stream
The Rolling Effectiveness of Wing-Tip Ailerons as Determined by Rocket-Powered Test Vehicles and Linear Supersonic Theory
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