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):

Report Date:

1978-11-01

Pagination or Media Count:

3.0

Abstract:

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE