Accession Number : ADA952046

Title :   3-Dimensional Smoke Tunnel Tests of the Flow around a Model of the Grumman F11F1,

Corporate Author : PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING

Personal Author(s) : Hazen, D. C. ; Willauer, W. R.

Report Date : JUN 1956

Pagination or Media Count : 26

Descriptors :   *THREE DIMENSIONAL FLOW, AIRCRAFT MODELS, WING BODY CONFIGURATIONS, FLOW FIELDS, SWEPTBACK WINGS, SUBSONIC WIND TUNNELS, WIND TUNNEL TESTS, SMOKE, FLOW VISUALIZATION.

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE