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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Flying qualities of a high-performance personal-owner airplane
Drag Measurements of a Swept-Back Wing Having Inverse Taper as Determined by Flight Tests at Supersonic Speeds
Determination of vortex paths by series expansion technique with application to cruciform wings
Pumping Characteristics for Several Simulated Variable-Geometry Ejectors With Hot and Cold Primary Flow
Pumping Characteristics for Several Simulated Variablegeometry Ejectors With Hot and Cold Primary Flow
Lateral Stability and Control Measurements of a 0.0858-Scale Model of the Lockheed XF-104 Airplane at Transonic Speeds
The development and application of high-critical-speed nose inlets
Experimental investigation of thrust augmentation of axial-flow-type 4000-pound-thrust turbojet engine by water and alcohol injection at compressor inlet
Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation
A Preliminary Investigation at Mach Number 1.91 of a Diffuser Employing a Pivoted Cone to Improve Operation at Angle of Attack
An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils
Free-Spinning Tunnel Tests of a 1/20-Scale Model of the McDonnell XF3H-1 Airplane : TED No. NACA DE 343
An Investigation of the Characteristics of an Unswept Wing of Aspect Ratio 4.01 in the Langley 8-Foot High-Speed Tunnel
Development of Metal-Bonding Adhesive FPL-710 With Improved Heat-Resistant Properties
Some Effects of Fuselage Interference, Wing Interference, and Sweepback on the Damping in Roll of Untapered Wings as Determined by Techniques Employing Rocket-Propelled Vehicles
Altitude operational characteristics of a prototype model of the J47D (RX1-1 and RX1-3) turbojet engines with integrated electronic control
Tests of Air Valves for Intermittent-Jet Engines at Speeds of 20 and 25 Cycles Per Second
Ground Simulator Studies of the Effects of Valve Friction, Stick Friction, Flexibility, and Backwash on Power Control System Quality
Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components
Effects of internal configuration on afterburner shell temperatures
Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and flame holders on J35 turbojet engine
Altitude Performance of AN-F-58 Fuels in British Rolls-Royce Nene Single Combustor
Exploratory Investigation of the Effect of Wing Slots and Leading-Edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Fuselage Configuration
Characteristics of Five Propellers in Flight
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