Accession Number : ADB050858

Title :   Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Casing Vortex Generator Configuration 'B' (Configuration 1B).

Descriptive Note : Interim technical rept. 1 Mar 76-1 Jul 77,

Corporate Author : AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH

Personal Author(s) : Wennerstrom, Arthur J. ; Law, C. Herbert ; DeRose, Robert D. ; Gurecki, Daniel J. ; Strain, Efren C.

Report Date : JUN 1980

Pagination or Media Count : 105

Abstract : For abstract see AD B050 857L.

Descriptors :   *AXIAL FLOW COMPRESSORS, *VORTEX GENERATORS, TURBOJET ENGINES, TURBOJET INLETS, AXIAL FLOW COMPRESSOR BLADES, TRANSONIC FLOW, COMPRESSOR ROTORS, TABLES(DATA), COMPUTER PRINTOUTS.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE