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- Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45©� high-wing model oscillating in yaw
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance
- Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
- Experimental investigation of the simulation of atmospheric entry of ballistic missiles
- Performance of basic XJ79-GE-1 turbojet engine and its components
- 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
- 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