Accession Number : AD0164379
Title : Wing and Thrust Augmentor.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : VON Ohain,Hans J. P. ; Campbell,William S.
Report Date : 03 APR 1973
Pagination or Media Count : 10
Abstract : The invention relates to aircraft wings in which there is combined therewith a jet propulsion means with thrust augmentation and in which the induced mass flow is derived from airflow over the wing surface including the boundary layer.
Descriptors : *Thrust augmentor nozzles, *Patents, Thrust augmentation, Thrust vectoring, Airfoils, Air flow
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE