Accession Number : AD0005535


Title :   COMPARISON OF THEORETICALLY AND EXPERIMENTALLY DETERMINED EFFECTS OF OXIDE COATINGS SUPPLIED BY FUEL ADDITIVES ON UNCOOLED TURBINE-BLADE TEMPERATURE DURING TRANSIENT TURBOJET-ENGINE OPERATION


Descriptive Note : Research memo.


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


Personal Author(s) : Schafer, Jr , Louis J ; Stepka, Francis S ; Brown, W B


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/005535.pdf


Report Date : 30 Mar 1953


Pagination or Media Count : 50


Descriptors :   *GAS TURBINE BLADES , FUEL ADDITIVES , TEMPERATURE , DEPOSITS


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE