Hostname: page-component-8448b6f56d-sxzjt Total loading time: 0 Render date: 2024-04-19T23:07:46.562Z Has data issue: false hasContentIssue false

Spin induced aerodynamic flow conditions on full-scale aeroplane wing and horizontal tail surfaces

Published online by Cambridge University Press:  27 January 2016

R. I. Hoff*
Affiliation:
Brunel Flight Safety Laboratory, School of Engineering and Design, Brunel University, Uxbridge, Middlesex, UK
G. B. Gratton*
Affiliation:
Brunel Flight Safety Laboratory, School of Engineering and Design, Brunel University, Uxbridge, Middlesex, UK

Abstract

The aerodynamic flow conditions on wings and tail surfaces due to the rotational motion of a spinning aeroplane have been investigated in a full-scale spin flight research programme at the Brunel Flight Safety Laboratory. The wing upper surface vortex has been visualised using smoke and tufts on the wing of a Slingsby Firefly. The flow structures on top of both wings, and on top of the horizontal tail surfaces, have also been studied on a Saab Safir. The development of these rotational flow effects has been related to the spin motion and the effect on the spin dynamics has been studied and discussed. Evidence suggests that the turbulent wake from the wing upper surface vortex impinges the tail of the aircraft during the spin entry. It is hypothesised that the turbulent flow structure on the outside upper wing surface is due to additional accelerations induced by the rotational motion of the aeroplane. Furthermore, the lightening in stick force during spin entry and the apparent increase in push force required for spin recovery corresponds to the observed change in flow condition on the horizontal tail. The difference in pressure on the upper and lower horizontal tail surfaces have been measured using differential pressure sensors, and the result corresponds both with the observed flow conditions and earlier research results from NASA.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 2013 

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 Sobie, B.PICTURE: Flight gets first look at redesigned SkyCatcher, Flightglobal.com, Business & GA Article, 03/02/09.Google Scholar
2. Trimble, S. SkyCatcher future in doubt after second flight test crash, Flightglobal.com, News Article, 20/03/09.Google Scholar
3. Fox, L.A. Lancair 400 Spin Testing and Spin Chute Release Failure, Proceedings of the 48th Annual SETP Symposium, 2004.Google Scholar
4. Roberts, S.C. Flight Test Lessons Learned from the Spinning Trials of the Gippsland GA-8 Single Engine General Aviation Aircraft, Proceedings of the 44th Annual SETP Symposium, 2000.Google Scholar
5. Sling LSA Prototype Lost During Spin Testing, EAA News, 25 February 2010.Google Scholar
6. South African Civil Aviation Authority, Aircraft Accident Report and Executive Summary, Sling, ZU-TAF, Ref. CA/18/2/3/8756.Google Scholar
7. Hoff, R.I. The Challenges of Light Aeroplane Spin Testing & Research, 4th European Flight Test Safety Workshop, London, UK, 28 September 2010.Google Scholar
8. Hoff, R.I. and Gratton, G.B. Camera tracking and qualitative airflow assessment of a 2-turn erect spin, Aeronaut J, May 2012, 116, (1179).Google Scholar
9. Stinton, D. Flying qualities and flight testing of the airplane, AIAA, Reston, VA, USA, ISBN 1-56347-274-0, 1996.Google Scholar
10. Bowman, J.S. Jr Summary of spin technology as related to light General-Aviation Airplanes, NASA TN D-6575, Washington DC, USA, December 1971.Google Scholar
11. Burk, S.M. Jr and Bowman, J.S. Jr and White, W.L. Spin-tunnel investigation of the spinning characteristics of typical Single-Engine General Aviation Airplane Designs. I – Low-wing model A: Effects of tail configurations, NASA Technical Paper 1009, September 1977.Google Scholar
12. Bowman, J.S. Jr, Hultberg, R.S. and Martin, C.A. Measurements of Pressures on the Tail and Aft Fuselage of an Airplane Model During Rotary Motions at Spin Attitudes, NASA Technical Paper 2939, 1989.Google Scholar
13. Brown, A.P. Dillon, J. Craig, G. and Erdos, R. Flight Manoeuvre and Spin Characteristics of the Harvard Mk 4: Application to Human Factors Flight Research, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Providence, Rhode Island, USA, 16-19 August 2004, 2004-4815.Google Scholar
14. Fisher Del, D.F., Frate, J.H. and Richwine, D.M. In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack, NASA TM-4193, May 1990.Google Scholar
15. Davis, M.C. and Saltzman, J.A. In-Flight Wing Pressure Distributions for the NASA F/A-18A High Alpha Research Vehicle, NASA TP-2000-209018, March 2000.Google Scholar
16. Comet, Smoke Signals for Parachutists, Data Sheet, Issue 24 April 2003.Google Scholar
17. MTi-G User Manual and Technical Documentation, Xsens Technologies B.V., Document MT0137P, Revsion H, 15 October 2010.Google Scholar
18. Muller, D. and Pommera, G.Spinning the modified ROBIN R2160, Cockpit, The Society of Experimental Test Pilots, April/May/June 1999.Google Scholar
19. Pitot-Static System PSS-8, Interface Definition Document, Simtec Buergel AG, Issue 1, 28 August 2012 Google Scholar
20. Private correspondance with Simtec Buergel AG, 21 November 2012.Google Scholar
21. Airplane Manual SAAB SAFIR 91B-2, Description, Control Surfaces, 3-4.Google Scholar
22. Pettersen, S. Weather Analysis and Forecasting, Second Edition, 1, Motion and Motion Systems, McGraw-Hill, 1956.Google Scholar
23. Meriam, J.L. and Kraige, L.G. Engineering Mechanics, Dynamics, 1993, 2, 3rd ed, ISBN 0-471-59273-0.Google Scholar
24. Letnik, D. and Dickinson, M.H. Biofuiddynamic scaling of flapping, spinning, and translating fns and wings, J Experimental Biology, 5 February, 2009, (212), pp 26912704.Google Scholar