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NACA Research Memorandums
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Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels
Fuel investigation in a tubular-type combustor of a turbojet engine
Investigation of shock diffusers at Mach number 1.85 3: multiple-shock and curved-contour projecting cones
Measurements of Aerodynamic Characteristics of a 35 Degree Sweptback NACA 65-009 Airfoil Model With 1/4-Chord Plain Flap by the NACA Wing-Flow Method
Preliminary investigation of spoiler lateral control on a 42 degree sweptback wing at transonic speeds
Estimate of Hull-Weight Change with Varying Length-Beam Ratio for Flying Boats
Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe
Aerodynamic Characteristics of a 45 Degree Swept-Back Wing With Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
Combustion-efficiency investigation of special fuels in single tubular-type combustor at simulated altitude conditions
High-speed wind-tunnel investigation of the effects of compressibility on a pitot-static tube
Low-Speed Investigation of a Small Triangular Wing of Aspect Ratio 2.0 1 The Effect of Combination With a Body Revolution and Height Above a Ground Plane
Free-Flight Investigation of Fullspan, 0.2 Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Taper, Aspect Ratio, and Section-Thickness Ratio
A Torsional Stiffness Criterion for Preventing Flutter of Wings of Supersonic Missiles
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
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