Accession Number : AD0164647
Title : Aerodynamic Nozzles in Rectangular Duct.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Quinn,Brian P.
Report Date : 15 JAN 1974
Pagination or Media Count : 4
Abstract : The patent relates to a rectangular duct having a gas flow therethrough wherein there is a tendency for the gas flow to separate from a wall of the duct. An aerodynamic nozzle is positioned adjacent the wall that results in a downwash of gas which deters separation.
Descriptors : *Thrust augmentor nozzles, *Patents, Short takeoff aircraft, Thrust augmentation, Ducts, Aerodynamics, Airfoils
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE