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)
Sea King Flight Tests Pitot-Static Probe and Directional Vane Instrumentation
1981
26 pages
Report
No indication
English
Aircraft , Aerodynamics , Pitot tubes , Guide vanes , Helicopters Airspeed indicators , Foreign technology , Booms(Equipment) , Probes , Static pressure , Air flow , tic pressure , Flight instruments , Angle of attack , Position(Location) , Error analysis , Sideslip , Pitch(Motion) , Air towed , Dynamic pressure , Noses , Calibration , Wind tunnel tests , Rotary wing aircraft , Flight testing , Sea King aircraft , MK-50 aircraft
Pitot-Static Puzzles Relearning lessons in instrumentation basics
British Library Online Contents | 2003
|Comparative tests of pitot-static tubes
Engineering Index Backfile | 1935
|Comparative tests of pitot-static tubes
TIBKAT | 1935
|C-141A Pitot-Static System Calibration Tests
NTIS | 1976
|NTRS | 1991
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