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NACA Research Memorandums
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A fuel-distribution control for gas-turbine engines
High-Speed Wind-Tunnel Investigation of a Flying-Boat Hull With High Length-Beam Ratio
Initial Flight Test of the NACA FR-1-A, a Low-Acceleration Rocket-Propelled Vehicle for Transonic Flutter Research
Investigation of Effects of Several Fuel-Injection Locations on Operational Performance of a 20-Inch Ram Jet
Comparison of Hovering Performance of Helicopters Powered by Jet-Propulsion and Reciprocating Engines
Preliminary Free-Flight Investigation of the Effect of Airfoil Section on Aileron Rolling Effectiveness at Transonic and Supersonic Speeds
The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model
Ice protection of turbojet engines by inertia separation of water 2: single-offset-duct system
Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift
Preliminary investigation of combustion in flowing gas with various turbulence promoters
Free-Spinning Characteristics of a 1/21-Scale Model of the Douglas AD-2W Airplane: TED No. NACA DE329
Investigation of wing characteristics at a Mach number of 1.53 2: swept wings of taper ratio 0.5
A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
Equations for the Design of Two-Dimensional Supersonic Nozzles
Effect of Aerodynamic Hysteresis on Critical Flutter Speed at Stall
Effect of Centrifugal Force on Critical Flutter Speed on a Uniform Cantilever Beam
High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane: D-588-1 Speed-Reduction Brake and Symmetrical-Profile Wing Characteristics
Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 2: effects of slots upon an inlet enclosing 61.5 percent of the maximum circumference of the forebody
Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degree Sweptback Wing and Tail as Obtained by the Transonic-Bump Method
Ice protection of turbojet engines by inertia separation of water 3: annular submerged inlets
Internal-Film Cooling of Rocket Nozzles
Limited measurements of static longitudinal stability in flight of Douglas D-558-1 airplane (BuAero No. 37971)
The Effectiveness at High Speeds of a 10-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section
Investigation of wing characteristics at a Mach number of 1.53 3: unswept wings of differing aspect ratio and taper ratio
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