Accession Number : ADA952405

Title :   Wind Tunnel Tests for Hughes Aircraft Co. in the 5 x 4 Wind Tunnel (Second Series),

Corporate Author : PRINCETON UNIV N J JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Perkins,C. D.

Report Date : 1949

Pagination or Media Count : 19

Descriptors :   *Engine nacelles, Helicopter rotors, Rotor blades(Rotary wings), Aerodynamic characteristics, Wind tunnel tests

Subject Categories : Aerodynamics
      Helicopters

Distribution Statement : APPROVED FOR PUBLIC RELEASE