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Accession Number:
AD0102311
Title:
INTERNAL PERFORMANCE CHARACTERISTICS OF SHORT CONVERGENT-DIVERGENT EXHAUST NOZZLES DESIGNED BY THE METHOD OF CHARACTERISTICS
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH GLENN RESEARCH CENTER
Report Date:
1956-07-24
Abstract:
An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.
Descriptive Note:
Research memo.
Pages:
0021
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
1.27MB
