Accession Number:
AD0742994
Title:
Wind Tunnel Test Results on a Flight Path Accelerometer at Subsonic and Supersonic Speeds
Descriptive Note:
Final rept. 6 Dec 1971-24 Jan 1972
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Personal Author(s):
Report Date:
1972-06-01
Pagination or Media Count:
18.0
Abstract:
A test program was conducted to obtain the damping characteristics of the vanes and to provide a flow calibration of a newly developed flight path accelerometer FPA. After earlier calibration results identified an interference problem from the sideslip vane strut on the angle-of-attack vanes, the sideslip vane was moved rearward, necessitating additional calibration tests. Results are reported.
Descriptors:
Subject Categories:
- Test Facilities, Equipment and Methods