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Impact Theory for Seaplane Landings

Description: Note presenting an analysis of a step landing of a seaplane on smooth water by solving Newton's differential equation of motion. Formulas are developed for the maximum acceleration, the maximum draft, and the draft at the instant of maximum acceleration.
Date: October 1947
Creator: Benscoter, Stanley U.
Partner: UNT Libraries Government Documents Department

Analysis of Multicell Delta Wings on Cal-Tech Analog Computer

Description: From Introduction: "The main purpose of this paper is to present the results of measurements made on the Cal-Tech computer. The diagrams present only a small portion of the data which were obtained from the computer and which are given in complete form in the tables."
Date: December 1, 1953
Creator: MacNeal, Richard H. & Benscoter, Stanley U.
Partner: UNT Libraries Government Documents Department