National Advisory Committee for Aeronautics (NACA) - 2 Matching Results

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Analytical investigation of acceleration restriction in a fighter airplane with an automatic control system

From Introduction: "In the present report, consideration is given to certain features intended to improve the accleration-limiting characteristics of a normal-accleration control system."

Date: January 1958

Creator: Matthews, James T., Jr.

Item Type: Report

Partner: UNT Libraries Government Documents Department

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An analytical investigation of airplane spin-recovery motion by use of rotary-balance aerodynamic data

From Introduction: "Many investigations have been made in the Langley 20-foot free-spinning tunnel in which the natures of airplane spins and recoveries have been determined experimentally with dynamically scaled-down models. The results of some of these investigations are presented in references 1 to 5."

Date: June 1954

Creator: Scher, Stanley H.