Accession Number:
AD0735066
Title:
Effect of Flow Discontinuities on Oscillatory Pressures Measured in Supersonic Wind Tunnels,
Descriptive Note:
Corporate Author:
NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)
Personal Author(s):
Report Date:
1969-10-13
Pagination or Media Count:
3.0
Abstract:
The effect of wind-tunnel flow discontinuities, which previously was considered to be a serious obstacle in measuring oscillatory surface pressures at supersonic speeds, was investigated. Results are reported for a particular nozzle in one tunnel.
Descriptors:
Subject Categories:
- Test Facilities, Equipment and Methods