NASA NTRS · 19920000108
Flow Over A Simplified-Rocket-Shaped Body
Abstract
Report describes observations of supersonic flow of air over cylindrical body capped by hemisphere at its head and flared to cone at its tail end. Study prompted by need for greater aircraft control at high angles of attack.
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Schiff, Lewis B., Meade, Andrew J., Jr.. 1992-02-01. Flow Over A Simplified-Rocket-Shaped Body. https://ntrs.nasa.gov/citations/19920000108
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