Flight Investigation at High-subsonic, Transonic, and Supersonic Speeds to Determine Zero-lift Drag of Fin-stabilized Bodies of Revolution Having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter
Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3
Flight Investigation of the Drag of Round-nosed Bodies of Revolution at Mach Numbers from 0.6 to 1.5 Using Rocket-propelled Test Vehicles
Flight Investigation at Mach Numbers from 0.8 to 1.5 to Determine the Effects of Nose Bluntness on the Total Drag of Two Fin-stabilized Bodies of Revolution
Effects of Stabilizing Fins and a Rear-support Sting on the Base Pressures of a Body of Revolution in Free Flight at Mach Numbers from 0.7 to 1.3
Flight Investigations at High-subsonic, Transonic, and Supersonic Speeds to Determine Zero-lift Drag of Fin-stabilized Bodies of Revolution Having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter
Flight Investigations at High-subsonic, Transonic, and Supersonic Speeds to Determine Zero-lift Drag of Fin-stabilized Bodies of Revoliution Having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter
Le développement de la connaissance spatiale et applications aux grands environnements : revue-critique