Hostname: page-component-848d4c4894-8bljj Total loading time: 0 Render date: 2024-07-02T19:53:59.164Z Has data issue: false hasContentIssue false
  • English
  • Français

New rotary rig at RAE and experiments on HIRM*

Published online by Cambridge University Press:  04 July 2016

C. O. O’Leary  and
E. N. Rowthorn
C. O. O’Leary
Affiliation:
Royal Aircraft Establishment, Aerodynamics Department, Bedford MK41 6AE
E. N. Rowthorn
Affiliation:
Royal Aircraft Establishment, Aerodynamics Department, Bedford MK41 6AE
Get access Rights & Permissions [Opens in a new window]

Summary

A rig for measurement of forces and moments due to continuous rate of roll has been commissioned at RAE Bedford. Tests have been made on a High Incidence Research Model (HIRM) in two wind tunnels at M = 0·2, 0·4 and 0·7. At present models can be tested up to 40° angle of attack at rotational speeds up to 350 rpm.

Tests on HIRM included an investigation of configuration and Reynolds number effects. Results are compared with similar data from tests with another rolling rig and from small amplitude oscillatory tests.

Type
Research Article
Information
The Aeronautical Journal , Volume 90 , Issue 900 , December 1986 , pp. 399 - 409
Copyright
Copyright © Royal Aeronautical Society 1996 

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.)

Footnotes

*

Paper originally presented at AGARD Symposium on Unsteady Aerodynamics, Fundamentals and Applications to Aircraft Dynamics, Gottingen, W. Germany, 6th-9th May 1985, and published in AGARD CP-386.

References

1. Moss, G. F., Ross, A. Jean and Butler, G. F. A programme of work on the flight dynamics of departure using a high incidence research model (HIRM). RAE Technical Memorandum Aero 1950. 1982.Google Scholar
2. Allen, P. J. P. Large scale rolling rig tests on the RAE Model 2130 (HIRM 2) in the BAe Warton 5.5 m Low Speed Wind Tunnel. BAe Report AXR 103. 1983.Google Scholar
3. Mathews, A. W. The feasibility study, design, manufacture, commissioning and technique development of a rolling rig for the measurement of dynamic derivatives. Part 1: Design and manufacture of the rig, drive system, data acquisition and control system and calibration equipment. BAe Report AXR 60, Pt 1, 1978.Google Scholar
4. Ross, A. Jean and Reid, G. E. A. The development of mathematical models for a high incidence research model. Part 1: Analysis of static aerodynamic data. RAE Technical Report 83037. Google Scholar