Accession Number : AD0101949


Title :   THE TWO DIMENSIONAL INFLOW CONDITIONS FOR A SUPERSONIC COMPRESSOR WITH CURVED BLADES


Corporate Author : AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OH


Personal Author(s) : LEVINE, PHILLIP


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/101949.pdf


Report Date : May 1956


Pagination or Media Count : 35


Descriptors :   *AXIAL FLOW COMPRESSORS , SUPERSONIC FLOW


Subject Categories : Hydraulic and Pneumatic Equipment


Distribution Statement : APPROVED FOR PUBLIC RELEASE