Accession Number : ADA952095

Title :   The Flow at the Rear of a Two-Dimensional Supersonic Airfoil,

Corporate Author : PRINCETON UNIV NJ JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Kahane, A. ; Lees, Lester

Report Date : 01 JUN 1947

Pagination or Media Count : 13

Descriptors :   *SUPERSONIC AIRFOILS, *TWO DIMENSIONAL FLOW, TRAILING EDGES, FREE STREAM, FLOW FIELDS, TRAILING CONTROL SURFACES, FLAT PLATE MODELS, THICKNESS.

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE