Accession Number:

ADD005006

Title:

Finned Surface Cooled Nozzle.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Report Date:

1978-03-28

Pagination or Media Count:

15.0

Abstract:

This patent describes an air-cooled, variable-throat, convergent-divergent nozzle for a turbojet engine.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE