Accession Number:

ADA277575

Title:

Hypervelocity Tunnel 9 Mach 8 Calibration

Descriptive Note:

Corporate Author:

NAVAL SURFACE WARFARE CENTER DAHLGREN DIV SILVER SPRING MD

Personal Author(s):

Report Date:

1994-03-10

Pagination or Media Count:

43.0

Abstract:

This report documents the Mach 8 Calibration test program WTR 1614 performed in the Navys Hypervelocity Wind Tunnel Tunnel 9. This was an in- house calibration test effort. Free stream flow field measurements were obtained for the Mach 8 nozzle, covering a wide range of Reynolds numbers. The calibration included running very low Reynolds numbers, not previously calibrated at Mach 8, as well as running at the current maximum supply conditions for Mach 8. The test period was 18 to 23 December 1992, with a total of five runs. Results from this test entry were combined with previous Mach 8 calibration data in the final analysis. Previous calibration data were taken when Mach 8 was originally brought on-line in December of 1988. The maximum supply conditions were lower during the original calibration than are currently available. However, data from this most recent calibration reveal that high quality uniform flow still exists and that deviations in core flow field parameters are comparable with other Tunnel 9 calibration data taken to date. Calibration, Wind Tunnel, Mach 8, Hypersonics, NSWC Tunnel 9.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE