Accession Number : ADA952981

Title :   Project SQUID, Two-Dimensional Supersonic Wind Tunnel Simulation of the Flow Over the External Surface of Ducted Bodies with and without Spillover,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Kamrass,M.

Report Date : 30 JUN 1947

Pagination or Media Count : 24

Descriptors :   *Airfoils, *Wind tunnel tests, Supersonic wind tunnels, Aerodynamic drag, Leading edges, Pressure measurement, Aerodynamic forces

Subject Categories : Aircraft
      Test Facilities, Equipment and Methods
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE