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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 Research Memorandums
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National Advisory Committee for Aeronautics Collection
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High-Altitude Performance of an Experimental Turbular Prevaporizing Combustor
Investigation to Mach number 2.0 of shock-positioning control systems for a variable-geometry inlet in combination with a J34 turbojet engine
Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle Upon the Pressure of the Base Annulus of a Body of Revolution
The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane
Low-Speed Measurements of Rolling and Yawing Stability Derivatives of a 60 Degree Delta-Wing Model
Lift and drag characteristics of the Douglas X-3 research airplane obtained during demonstration flights to a Mach number of 1.20
A preliminary investigation of the use of circulation control to increase the lift of a 45 degree sweptback wing by suction through trailing-edge slots
Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6.8 x 10(6)
A Thermal Equation for Flame Quenching
A Survey of Background and Aircraft Noise in Communities Near Airports
Operating Characteristics of an Acceleration Restrictor as Determined by Means of a Simulator
Analytical determination of the mechanism of an airplane spin recovery with different applied yawing moments by use of rotary-balance data
Approximate effect of leading-edge thickness, incidence angle, and inlet mach number on inlet losses for high-solidity cascades of low cambered blades
Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates
Some Measurements of Noise From Three Solid-Fuel Rocket Engines
Design Considerations for Wings Having Minimum Drag Due to Lift
Use of a Hot-Wire Anemometer in Shock-Tube Investigations
On the Analysis of Linear and Nonlinear Dynamical Systems From Transient-Response Data
A Theoretical Investigation of the Short-Period Dynamic Longitudinal Stability of Airplane Configurations Having Elastic Wings of 0 Degree to 60 Degrees Sweepback
An investigation of a wing-propeller configuration employing large-chord plain flaps and large-diameter propellers for low-speed flight and vertical take-off
Mechanical Properties at Room Temperature of Four Cermets of Tungsten Carbide with Cobalt Binder
Boundary-layer transition at Mach 3.12 with and without single roughness elements
Theoretical Calculations of the Lateral Stability Derivatives for Triangular Vertical Tails with Subsonic Leading Edges Traveling at Supersonic Speeds
Electrical Analogies for Stiffened Shells With Flexible Rings
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