Accession Number:

AD0620074

Title:

A SUPERSONIC AXISYMMETRICAL NOZZLE FOR WIND TUNNELS,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1965-06-29

Pagination or Media Count:

6.0

Abstract:

For the purpose of lowering the thermal stresses and temperature deformations which distort the configuration of the flow part the uncooled nozzle is designed in bracket fashion.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE