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

Report Date:

1980-06-01

Pagination or Media Count:

105.0

Abstract:

For abstract see AD B050 857L.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE