Accession Number:

ADA162018

Title:

Pressure Measurements on Five Miniature Mach/Flow Angularity Probes at Mach Numbers 1.76, 2.0, 3.0 and 5.0

Descriptive Note:

Final rept. for the period ending 20 Mar 1983

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN

Report Date:

1983-05-01

Pagination or Media Count:

29.0

Abstract:

Pressure measurements were obtained on five miniature Machflow angularity MFA probes which were developed at AEDC as part of an on-going probe development effort. These measurements will be correlated with Mach number and known flow angle in order to calibrate these probes. Secondary objectives were to test a hot-film anemometer and three pitot acoustic probes for durability, and to examine the response of three ported dynamic pressure transducers located downstream of the tunnel test section.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE