A MACH NUMBER MONITOR FOR A TRANSONIC WIND-TUNNEL.
Abstract
The report describes the Mach number monitor installed in the 3 ft tunnel for use in setting and holding constant the test Mach number at transonic speeds. A Wheatstone bridge is employed to compare the ratio of resistance analogues of static pressure and total pressure with a four-digit target ratio. Unbalance is indicated in terms of error in mach number M. The instrument is accurate to 0.001 M over its useful range of M = 0.3 to 1.4 K also provides an electrical output which could be used for automatic control of tunnel speed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1967
- Accession Number
- AD0665811
Entities
People
- S. Barcroft
Organizations
- Royal Aircraft Establishment