Accession Number:

ADA046819

Title:

The SES Lift Fan Evaluation Rig.

Descriptive Note:

Final rept.,

Corporate Author:

DAVID W TAYLOR NAVAL SHIP RESEARCH AND DEVELOPMENT CENTER BETHESDA MD AVIATION AND SURFACE EFFECTS DEPT

Personal Author(s):

Report Date:

1977-02-01

Pagination or Media Count:

42.0

Abstract:

A test rig for the experimental evaluation of Surface Effect Ship SES lift fan models has been designed, fabricated, and integrated into one of the 8- by 10-foot subsonic wind tunnels at the David W. Taylor Naval Ship Research and Development Center DTNSRDC. Centrifugal and axial flow lift fan characteristics have been investigated under steady state as well as time-varying flow rate conditions. Fans of about 2 feet in diameter or less and up to 150 hp can be handled on the rig. Instrumentation includes transducers to measure pressure, power, and efficiency. Association with the rig is a digital data acquisition system capable of sampling data at rates of up to 12 KHZ. Author

Subject Categories:

  • Aircraft
  • Marine Engineering

Distribution Statement:

APPROVED FOR PUBLIC RELEASE