Hostname: page-component-7bb8b95d7b-5mhkq Total loading time: 0 Render date: 2024-09-12T10:38:22.487Z Has data issue: false hasContentIssue false
  • English
  • Français

An oscillatory method for the flight calibration of sideslip and incidence sensors

Published online by Cambridge University Press:  04 July 2016

B. R. A. Burns
B. R. A. Burns*
Affiliation:
British Aircraft Corporation Limited, Military Aircraft Division
Get access Rights & Permissions [Opens in a new window]

Extract

The local flow angles measured by incidence and sideslip probes mounted on aircraft differ in general from the free stream or ‘true’ values due to the flow field of the aircraft and of the sensors themselves.

This note describes a method of determining the correction factors by means of measurements made in oscillatory motion. The longitudinal short period mode is used for incidence calibration, the dutch roll for sideslip.

Type
Technical notes
Information
The Aeronautical Journal , Volume 77 , Issue 754 , October 1973 , pp. 506 - 511
Copyright
Copyright © Royal Aeronautical Society 1973 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Bryant, and Gates, . Nomenclature of stability coefficients. R and M 1801.Google Scholar
2. Pinsker, . The static and dynamic response properties of incidence vanes with aerodynamic and internal viscous damping. RAE TN Aero 2833.Google Scholar
3. McLaren, . Calibration methods for the accurate assesment of the dynamic performance of some flight test instruments. RAE TN Aero 2914.Google Scholar
4. Boisson, . Etallonage d'Incidence et Derapage. AGARD Report 77.Google Scholar