Accession Number : AD0029121


Title :   EXPERIMENTAL INVESTIGATION OF ROTATING STALL AND BLADE VIBRATION IN THE AXIAL-FLOW COMPRESSOR OF A TURBOJET ENGINE


Descriptive Note : Research memo.


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


Personal Author(s) : HUPPERT, MERLE C ; CALVERT, HOWARD F ; MEYER, ANDRE J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/029121.pdf


Report Date : Apr 1954


Pagination or Media Count : 29


Descriptors :   *TURBOJET ENGINES , AXIAL FLOW COMPRESSOR BLADES , VIBRATION , STALLING


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE