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Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01

Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition

Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet

Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4

Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Preliminary studies of rolling-contact fatigue life of high-temperature bearing materials

Correlation of turbulent heat transfer in a tube for the dissociating system N204 reversibly yields 2N02

Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination

Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio

Performance of basic XJ79-GE-1 turbojet engine and its components

Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds

Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing


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