Accession Number:

ADP006048

Title:

Turbulence Measurement in Hypersonic Flow,

Descriptive Note:

Corporate Author:

COMPLERE INC PALO ALTO CA

Personal Author(s):

Report Date:

1987-11-01

Pagination or Media Count:

17.0

Abstract:

An assessment has been made of the potential for hot wire and laser anemometer measurements of turbulent fluctuations in hypersonic flow fields. The results of experiments conducted in the AFWAL M6 High Reynolds Number Wind Tunnel are reported and comparisons made with previous hot wire turbulence measurements.

Subject Categories:

  • Fluid Mechanics
  • Test Facilities, Equipment and Methods

Distribution Statement:

APPROVED FOR PUBLIC RELEASE