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NACA Research Memorandums
269
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NACA Research Memorandums
269
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1949
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1949
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NACA Research Memorandums
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Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine
Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio
Chordwise and Spanwise Loadings Measured at Low Speed on Large Triangular Wings
An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 3: Characteristics of Wing With Body and Vertical Tail
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle
Response of a Rotating Propeller to Aerodynamic Excitation
High Speed Stability and Control Characteristics of a 0.17-Scale Model of the McDonnell XF2H-1 Airplane (TED No. NACA DE 318)
Investigation of Internal Regenerative Fuel-Heating System for 20-Inch Ram Jet
The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator
Stability Results Obtained With Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89
Aerodynamic Characteristics of an 0.08-Scale Model of the Martin XB-51 Airplane at High Subsonic Speeds
Altitude-chamber performance of British Rolls-Royce Nene II engine 1: standard 18.75-inch-diameter jet nozzle
Preliminary Investigation of 3-Inch Slotted Transonic Wind-Tunnel Test Sections
Low-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
Performance of J33-A-21 and J33-A-23 Turbojet-Engine Compressors with Water Injection
Theoretical Investigation of the Dynamic Lateral Stability Characteristics of Douglas Design No. 39C, an Early Version of the X-3 Research Airplane
Effect of Air Cooling of Turbine Disk on Power and Efficiency of Turbine from Turbo Engineering Corporation TT13-18 Turbosupercharger
Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the McDonnell XF2H-1 Airplane
Spin and Recovery Characteristics of the Northrop XF-89 Airplane
Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins
Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane with Wing-Tip Tanks Installed
Survey of two-dimensional data on pitching-moment changes near maximum lift caused by deflection of high-lift devices
An Investigation of the Characteristics of an Unswept Wing of Aspect Ratio 4.01 in the Langley 8-Foot High-Speed Tunnel
Effects of wing-tip turrets on the aerodynamic characteristics of a typical bomber-wing model
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