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
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE