Accession Number : AD0102311


Title :   INTERNAL PERFORMANCE CHARACTERISTICS OF SHORT CONVERGENT-DIVERGENT EXHAUST NOZZLES DESIGNED BY THE METHOD OF CHARACTERISTICS


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH GLENN RESEARCH CENTER


Personal Author(s) : KRULL, H G ; BEALE, WILLIAM T


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/102311.pdf


Report Date : 24 Jul 1956


Pagination or Media Count : 21


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.


Descriptors :   *GAS TURBINE NOZZLES , PERFORMANCE(ENGINEERING) , REDUCTION , PRESSURE , NOZZLE GAS FLOW , EXHAUST NOZZLES , CONVERGENT DIVERGENT NOZZLES , DISTRIBUTION , THRUST


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE