Accession Number:

AD0773352

Title:

The Low Hub-Tip Ratio Supersonic Axial-Flow Compressor. Volume IV.

Descriptive Note:

Final rept. 1 Jul 71-30 Jun 72,

Corporate Author:

VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM) TURBOMACHINERY LAB

Personal Author(s):

• Breugelmans,Frans A. E.

Report Date:

1973-06-01

Pagination or Media Count:

55.0

Abstract:

The report describes the overall and detail performance of the Mach 2 supersonic rotor at 70, 84, 90 and 100 of the design speed. Author

Descriptors:

• BELGIUM
• STALLING
• INLET GUIDE VANES
• FLOW FIELDS
• COMPRESSOR COMPONENTS
• BLEED SYSTEMS
• SUPERSONIC FLOW

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE