Accession Number:

AD0603022

Title:

A HIGH SPEED COMPUTER TECHNIQUE TO DETERMINE NOZZLE CONTOURS FOR SUPERSONIC WIND TUNNELS.

Descriptive Note:

Mathematics dept. rept.,

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1964-05-04

Pagination or Media Count:

32.0

Abstract:

This report describes a computer program developed at the Naval Ordnance Laboratory to calculate contours for supersonic wind tunnel nozzles. Both two-dimensional and axi-symmetric flow is covered and the technique arises from the method of characteristics in the theory of solution of hyperbolic partial differential equations. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE