Flight investigation at high-subsonic, transonic, and supersonic speeds to determine zero-lift drag of bodies of revolution having fineness ratio of 6.04 and varying positions of maximum diameter
Description: Report presenting a flight investigation of rocket-powered models at high-subsonic, transonic, and supersonic speeds to determine the zero-lift drag of fin-stabilized bodies of revolution differing in maximum diameter. All bodies had 6.04 fineness ratio and cut-off sterns with equal base area. The most favorable location out of the 20-percent, 40-percent, and 60-percent positions were evaluated for different speeds.
Date: August 31, 1949
Creator: Katz, Ellis R.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department