AN EXPERIMENTAL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF SLENDER HYPERSONIC VEHICLES AT HIGH ANGLES OF ATTACK
NAVAL ORDNANCE LAB WHITE OAK MD
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Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 23 power law body and two ducted-cone configurations.
- Guided Missiles
- Fluid Mechanics