Accession Number:

AD0062509

Title:

Supersonic Nozzle Design

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1950-04-04

Pagination or Media Count:

10.0

Abstract:

An analytic methcd for designing nozzles is described herein. This method Nilsons allows for the nonuniformity of flow across the throat.

Descriptors:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE