Accession Number : ADA952109

Title :   Three-Dimensional Smoke Tunnel Investigations of the Fuselage Flow about a 1.5% Scale Model of the Douglas C-133A Airplane,

Corporate Author : PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING

Personal Author(s) : Hazen, D. C. ; Lehnert, R. F.

Report Date : NOV 1957

Pagination or Media Count : 37

Descriptors :   *VORTICES, *WAKE, *FUSELAGES, TURBULENCE, TAILS(AIRCRAFT), HORIZONTAL ORIENTATION, ANGLE OF ATTACK, YAW, SCALE MODELS, TEST FACILITIES, SMOKE.

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

Distribution Statement : APPROVED FOR PUBLIC RELEASE