Accession Number : AD0029122


Title :   REVIEW OF HIGH-PERFORMANCE AXIAL-FLOW-COMPRESSOR BLADE-ELEMENT THEORY


Descriptive Note : Research memo.


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


Personal Author(s) : Lieblein, Seymour


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/029122.pdf


Report Date : 06 Apr 1954


Pagination or Media Count : 39


Descriptors :   *AXIAL FLOW COMPRESSOR BLADES , THEORY , TRANSONIC CHARACTERISTICS


Subject Categories : Hydraulic and Pneumatic Equipment


Distribution Statement : APPROVED FOR PUBLIC RELEASE