An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds
Description: From Introduction: "The present paper introduces the approximate method by means of which it is possible to calculate the pressures in the tip region of a rectangular with a symmetrical circular-arc section to a higher degree of accuracy than is possible with the usual linear methods."
Date: October 1950
Creator: Czarnecki, K. R. & Mueller, James N.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department