The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow
Description:
Report presenting the results of an investigation to determine the effects of a small jet of air exhausting from the nose of an elliptical body of revolution upon boundary-layer transition and the viscous, pressure, and total drag of the forebody at three body stations at Mach number 1.62. The jet effects on body pressure, pressure variations, boundary-layer transition, and total drag are provided.
Date:
November 12, 1952
Creator:
Love, Eugene S.
Partner:
UNT Libraries Government Documents Department