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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Technical Reports
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NACA Research Memorandums
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NACA Technical Reports
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1950-1959
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National Advisory Committee for Aeronautics Collection
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Summary of NACA Research on Afterburners for Turbojet Engines
Preliminary Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 1/20-Scale Model of the McDonnell F4H-1 Airplane at Mach Numbers of 1.59, 1.89, and 2.09
Large-scale flight measurements of zero-lift drag at Mach numbers from 0.8 to 1.6 of a wing-body combination having an unswept 4.5 percent thick wing with modified hexagonal sections
Some Effects of Stator Cone Angle and Blade-Tip Leakage on 40 Percent Reaction Turbine Having Rotor-Blade Caps
Summary of NACA research on afterburners for turbojet engines
Performance of Compressor of XJ-41-V Turbojet Engine 6 - Analysis of Compressor Flow Choking
Measurements of the Longitudinal Stability and Control and Stalling Characteristics of a North American P-51H Airplane (AAF No. 4-64164)
Spatial Burnout in Water Reactors with Nonuniform Startup Distributions of Uranium and Boron
Effects of Taper Ratio on the Longitudinal Characteristics at Mach Numbers From 0.6 to 1.4 of a Wing-Body-Tail Combination Having an Unswept Wing of Aspect Ratio 3
Influence of end plates on lift and flow field of a canard-type control surface at a Mach number of 2.00
Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction
The Effect of a 4-Percent-High Spoiler on Buffeting Forces on a NACA 65(Sub 06)A004 Two-Dimensional Airfoil at Subsonic Mach Numbers
A flight and analog computer study of some stabilization and command networks for an automatically controlled interceptor during the final attack phase
Effects of sweep and taper on the longitudinal characteristics of an aspect ratio 3 wing-body combination at Mach numbers from 0.6 to 1.4
Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semicircular Air Inlet in the Root of a 45 Degree Sweptback Wing
An Investigation of the Effects of Rapid Skin Heating on Box Beams Loaded in Bending
Zero-Lift Drag of Several Conical and Blunt Nose Shapes Obtained in Free Flight at Mach Numbers of 0.7 to 1.3
Temperature Drops Through Liquid-Cooled Turbine Blades With Various Cooling-Passage Geometries
Wind-Tunnel Investigation at High Subsonic Speeds of the Effects of Wing-Mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined With a Fuselage
The Weathering of Aluminum Alloy Sheet Materials Used in Aircraft
A New Principle of Sound Frequency Analysis
Jet Propulsion for Airplanes
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