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NACA Research Memorandums
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NACA Research Memorandums
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1958
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NACA Research Memorandums
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1958
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Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane
Preliminary Transonic Flutter Investigation of Models of T-Tall of Blackburn NA-39 Airplane
Performance of an Isentropic, All-Internal-Contraction, Axisymmetric Inlet Designed for Mach 2.50
Design and Experimental Investigation of a Single-Stage Turbine With a Rotor Entering Relative Mach Number of 2
Preliminary Transonic Flutter Investigation of Models of T-Tail of Blackburn NA-39 Airplane
Investigation of the Performance and Internal Flow of a Variable-Area, Variable-Internal-Contraction Inlet at Mach Numbers of 2.00, 2.50, and 2.92
Effects of nose and afterbody modifications on aerodynamic characteristics of a body with and without a vertical tail at a Mach number of 2.01
Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane
Effects of shock-boundary-layer interaction on the performance of a long and a short subsonic annular diffuser
Jet effects on the base drag of a cylindrical afterbody with extended nozzles
An Exploratory Investigation at Mach Numbers of 2.50 and 2.87 of a Canard Bomber-Type Configuration Designed for Supersonic Cruise Flight
Experimental ablation cooling
Wind-tunnel investigation of the low-speed aerodynamic characteristics of a hypersonic glider configuration
The static and dynamic-rotary stability derivatives at subsonic speeds of a model of the X-15 research airplane
Effect of leading-edge-flap deflection on the wing loads, load distributions , and flap hinge moments of the Douglas X-3 research airplane at transonic speeds
Effect of screens in reducing distortion and diffusion length for a 'dump' diffuser at a Mach number of 3.85
Longitudinal and Lateral Stability and Control Characteristics and Vertical-Tail-Load Measurements for a 0.03-Scale Model of the Avro CF-105 Airplane at Mach Numbers of 1.60, 1.80, and 2.00
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