Accession Number : AD0028728


Title :   COMBUSTION PERFORMANCE OF TWO EXPERIMENTAL TURBOJET ANNULAR COMBUSTORS AT CONDITIONS SIMULATING HIGH-ALTITUDE SUPERSONIC FLIGHT


Descriptive Note : Research memo.


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


Personal Author(s) : ZETTLE, EUGENE V ; NORGREN, CARL T ; MARK, HERMAN


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/028728.pdf


Report Date : 26 Mar 1954


Pagination or Media Count : 32


Descriptors :   *TURBOJET ENGINES , HIGH ALTITUDE , SIMULATION , TEST EQUIPMENT


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE