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Modelling of the hose and drogue in air-to-air refuelling

Published online by Cambridge University Press:  04 July 2016

A. W. Bloy  and
M. M. Khan
A. W. Bloy
Affiliation:
Manchester School of Engineering, University of Manchester
M. M. Khan
Affiliation:
Manchester School of Engineering, University of Manchester
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Abstract

A static model of the hose and drogue used to provide data in a realtime flight simulation of air-to-air refuelling is presented. The model predicts (a) the interference effect of the flow around the nose of a combat receiver aircraft on the pre-contact position of the drogue and (b) the hose shape and the loads induced on the receiver probe during contact. The use of the static model in the pre-contact case is validated for a normal closure speed by comparison with the results from a small perturbation dynamic analysis. At higher closure speed the static model is found to be less satisfactory. In a typical receiver approach a movement of the drogue similar to the drogue radius is predicted.

Type
Research Article
Information
The Aeronautical Journal , Volume 106 , Issue 1055 , January 2002 , pp. 17 - 26
Copyright
Copyright © Royal Aeronautical Society 2002 

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References

1. Bradley, J. The handling and performance trials needed to clear an aircraft to act as a receiver during air-to-air refuelling, 1984, AGARD conference proceedings No 373 (Flight test techniques), Paper No 9.Google Scholar
2. Prothero, R.M. Air-to-air refuelling simulation - rapid progress reveals novel problems, 1986, International conference on advances in flight simulation visual and motion systems, 1986, London.Google Scholar
3. Eichler, J. Dynamic analysis of an in-flight refuelling system, AIAA J Aircr, 1978, 15, pp 311–318.Google Scholar
4. Henderson, J.F. and Ireland, B. Flight validation of the computer program CBAS (cable body airborne simulator), 1996, proceedings of the Institution of Mechanical Engineers, 1996, 210, pp 93–100.Google Scholar
5. Lea, K. The Aerodynamics of Air-to-air Refuelling, 1995, PhD thesis, University of Manchester.Google Scholar
6. Lewis, R.I. Vortex Element Methods for Fluid Dynamic Analysis of Engineering Systems, Cambridge University Press, 1991.Google Scholar