Mach-Number Measurement with Laser and Pressure Probes in Humid Supersonic Flow

This article presents the Mach-number measurement with laser and pressure probes in humid supersonic flow. A comparative study is describe here for pressure-probe and laser-induced thermal acoustics based Mach-number measurements versus humidity in the unitary plan wind tunnel.

Saved in:
Bibliographic Details
Published in:AIAA journal 2008-08, Vol.46 (8), p.2107-2109
Main Author: Herring, G. C
Format: Article
Language:English
Subjects:
Aerodynamics
Compressible flows
shock and detonation phenomena
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Instrumentation for fluid dynamics
Measurement
Physics
Reynolds number
Supersonic and hypersonic flows
Wind tunnels
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:This article presents the Mach-number measurement with laser and pressure probes in humid supersonic flow. A comparative study is describe here for pressure-probe and laser-induced thermal acoustics based Mach-number measurements versus humidity in the unitary plan wind tunnel.
ISSN:0001-1452
1533-385X
DOI:10.2514/1.36107