Accession Number : AD0030124


Title :   INVESTIGATION OF IMPULSE-TYPE SUPERSONIC COMPRESSOR WITH HUB-TIP RATIO OF 0.6 AND TURNING TO AXIAL DIRECTION 1 - PERFORMANCE OF ROTOR ALONE


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC


Personal Author(s) : WILCOX, WARD W


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/030124.pdf


Report Date : 06 May 1954


Pagination or Media Count : 47


Descriptors :   *COMPRESSOR ROTORS , SUPERSONIC FLOW , IMPELLERS


Subject Categories : Hydraulic and Pneumatic Equipment


Distribution Statement : APPROVED FOR PUBLIC RELEASE