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NACA Research Memorandums
41
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NACA Research Memorandums
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1953
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1953
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Investigations toward simplification of missile control systems
Stability and Control Characteristics at Low Speed of a Modified 1/10-Scale Model of the MX-1554A Design
Experimental and theoretical investigation of rotating-stall characteristics of single-stage axial-flow compressor with hub-tip ratio of 0.76
A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds
Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conductive to Low Transonic Drag Rise
Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers
Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle
Performance of a supersonic mixed-flow rotor with a swept leading edge and 0.52 inlet radius ratio
Effects of slot location and geometry on the flow in a square tunnel at transonic Mach numbers
The Variation of Atmospheric Turbulence With Altitude and Its Effect on Airplane Gust Loads
Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conducive to Low Transonic Drag Rise
Evaluation of effects of random permeability variations on transpiration-cooled surfaces
Investigation of a Chromium Plus Aluminum Oxide Metal-Ceramic Body for Possible Gas Turbine Blade Application
Investigation of an Axial-Flow Compressor Rotor Having Naca High-Speed Blade Sections (A(Sub 2)I(Sub 8B) Series) at Mean Radius Relative Inlet Mach Numbers Up to 1.13
A Method for Estimating the Rolling Moments Caused by Wing-Tail Interference for Missiles at Supersonic Speeds
Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range
Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01
Preflight Tests and Flight Performance of a 6.5-Inch Diameter Ram-Jet Engine
Low-speed static stability and control characteristics of a 1/4-scale model of the Bell X-1 airplane equipped with a 4-percent-thick, aspect-ratio-4, unswept wing
Some Effects of Leading-Edge Roughness on the Aileron Effectiveness and Drag of a Thin Rectangular Wing Employing a Full-Span Plain Aileron at Mach Numbers From 0.6 to 1.5
An Investigation at Mach Number 2.40 of Flap-Type Controls Equipped With Overhang Nose Balances
Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range From 0.5 to 0.95
An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings
Gust-Tunnel Investigation of the Effect of Leading Edge Separation on the Normal Accelerations Experienced by a 45 Degree Sweptback-Wing Model in Gusts
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