Accession Number : ADA955784

Title :   Correlation of Axial-Flow Compressor and Fan Cascade Deviation Angles by Analysis of Blade Surface Boundary Layer Characteristics.

Descriptive Note : Final rept. 1 May-30 Sep 78,

Corporate Author : IOWA STATE UNIV AMES DEPT OF MECHANICAL ENGINEERING

Personal Author(s) : Serovy, George K.

Report Date : NOV 1978

Pagination or Media Count : 3

Descriptors :   *AXIAL FLOW COMPRESSOR BLADES, BOUNDARY LAYER FLOW.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE