Sea King Flight Tests Pitot-Static Probe and Directional Vane Instrumentation

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)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1981
Accession Number
ADA109427

Entities

People

  • D. T. Hourigan
  • M. J. Williams

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Air Flow
  • Air Force
  • Aircrafts
  • Aspect Ratio
  • Calibration
  • Department Of Defense
  • Diameters
  • Dynamic Pressure
  • Dynamic Response
  • Flow
  • Frequency
  • Instrumentation
  • Measurement
  • Resonant Frequency
  • Static Pressure
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Oceanography.