Accession Number:
ADA109427
Title:
Sea King Flight Tests Pitot-Static Probe and Directional Vane Instrumentation
Descriptive Note:
Technical memo.
Corporate Author:
AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)
Personal Author(s):
Report Date:
1981-07-01
Pagination or Media Count:
25.0
Abstract:
A short description is given of the pitot-static pressure probe and vanes mounted on a nose boom for Sea King flight tests. Also described is a probe which was trailed below the aircraft to determine the position error of the boom probe. Results of wind tunnel calibrations of these probes are given. Author
Descriptors:
- *FOREIGN TECHNOLOGY
- *HELICOPTERS
- *PITOT TUBES
- *GUIDE VANES
- FLIGHT TESTING
- POSITION(LOCATION)
- PROBES
- PITCH(MOTION)
- AIR FLOW
- ANGLE OF ATTACK
- ERROR ANALYSIS
- WIND TUNNEL TESTS
- FLIGHT INSTRUMENTS
- SIDESLIP
- CALIBRATION
- AUSTRALIA
- NOSES
- STATIC PRESSURE
- DYNAMIC PRESSURE
- ROTARY WING AIRCRAFT
- BOOMS(EQUIPMENT)
- AIR TOWED
- AIRSPEED INDICATORS
Subject Categories:
- Aerodynamics
- Helicopters
- Flight Control and Instrumentation
- Test Facilities, Equipment and Methods