Accession Number:

AD0092632

Title:

A STUDY OF THE END WALL BOUNDARY LAYER IN AN AXIAL COMPRESSOR BLADE ROW

Descriptive Note:

Corporate Author:

MASSACHUSETTS INST OF TECH CAMBRIDGE GAS TURBINE LAB

Report Date:

1955-10-01

Pagination or Media Count:

62.0

Abstract:

Subject Categories:

  • Hydraulic and Pneumatic Equipment
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE