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Testing a new model of ram-air parachute inflation

Published online by Cambridge University Press:  04 July 2016

J. Potvin*
Affiliation:
Department of Science and Mathematics, Parks College of Engineering and Aviation, Saint Louis University, St Louis, Missouri, USA

Abstract

This paper reports on the experimental validation of a new model of slider-reefed ram-air parachute opening, using jump data collected by this investigator and others. The model is based on the parachute load equation of motion coupled with a new differential equation which describes the rate of change of the parachute's drag area. The model clearly identifies the important factors which determine the inflation peak load and opening time. It also features many scaling relationships useful for design work. Several predictions are shown to be design-independent. The experimental data used in this model validation were gathered during sport parachuting jumps performed by this author. Also used are data generated by the US Navy during tests of the MC-5, MT-1X/SL and MT-1XX parachutes. The experimental results and model predictions are found to agree within 20% accuracy over a wide range of opening speeds and deployment altitudes.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1997 

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References

1. Macha, J.M. A simple, approximate model of parachute inflation, AIAA Paper 93-1206, 1993, and references therein.Google Scholar
2. Strickland, J. and Higuchi, H. Parachute aerodynamics: an assessment of prediction capability, AIAA Paper 95-1531, 1995.Google Scholar
3. Peterson, C.W., Strickland, J.H. and Higuchi, H. The fluid dynamics of parachute inflation, Annu Rev Fluid Mech, 1996, 28, (361).Google Scholar
4. Knacke, T.W. Parachute Recovery Systems Design Manual, Santa Barabara, CA, 1992.Google Scholar
5. Poynter, D. The Parachute Manual, Volumes I and II, Santa Barabara, CA, 1992.Google Scholar
6. Lingard, J.S. A semi-empirical theory to predict the load-time history of and inflating parachute, AIAA Paper 84-0814.Google Scholar
7. Garrard, W.L. Application of inflation theories to preliminary parachute force and stress analysis, AIAA Paper 91-0862.Google Scholar
8. Lingard, J.S. Ram-air parachute design, Precision Aerial Delivery Seminar, 13th AIAA Aerodynamic Decelerator Systems Technology Conference, Clearwater Beach, (Report unpublished), May 1995, and references therein.Google Scholar
9. Lingard, J.S. Gliding parachutes, Report PR-409, Para Publishing, Santa Barbara, CA, and references therein.Google Scholar
10. Garrard, W.L., Tezduyar, T.E., Aliabadi, S.K., Kalro, V., Luker, J. and Mittal, S. Inflation analysis of ram air inflated gliding parachutes, AIAA Paper 95-1565.Google Scholar
11. Aliabadi, S.K., Garrard, W.L., Kalro, V., Mittal, S., Tezduyar, T.E. and Stein, K.R. Parallel finite element computation of the dynamics of large ram air parachutes, AIAA paper 95-1581.Google Scholar
12. Potvin, J. Deployment model for slider-reefed ram-air parachutes, AIAA Paper 95-1564.Google Scholar
13. Sanborn, J.M. A Study into the proper body position to minimise parachute opening shock, ME-489 Undergraduate Advanced Individual Project Report, USMA, May 1990. Unpublished.Google Scholar
14. Lingard, J.S. The effects of added mass on parachute inflation force coefficients, AIAA Paper 95-1561.Google Scholar
15. Strickland, J.H. and Macha, J.M. Preliminary characterisation of parachute wake recontact, J Aircraft, 1990, 27, pp 501506.Google Scholar
16. Evans, J.H. Dimensional analysis and the Buckingham PI theorem, Am J Phys, 1972, 40, 1815.Google Scholar
17. Baldwin, D.A., Kolb, L.M., Wittendorfer, K.E. and Nagel, L. Qualification tests for service use of the USMC MC-5 ram air parachute assembly (free fall and static line configuration), Naval Air Warfare Center Weapons Division, Report NAWCWPNS TM 7330 (unplublished), November l992.Google Scholar
18. Kolb, L.M. and Nagel, L. Service use tests of the MT-1XS/SL ram Air parachute assembly Naval Air Warfare Center Weapons Division, Report NAWCWPNS TM 7803 (unpublished) May 1995.Google Scholar
19. Aero Systems Program Office, Advanced Parachute Technology (APT) Testing Results of the Para-Flite Model MT-1XX, February 1992, unpublished.Google Scholar
20. Potvin, J. and Montanez, R. The Parks College ram-air parachute deployment 1994-95 study, Parks College Report PARKS-SM-1996-01, January 1996, unpublished. Potvin, J., Montanez, R. and Peek, G. The Parks College ram-air parachute deployment study: a status report, AIAA Paper 91-1426.Google Scholar
21. Anderson, D.R., Sweeney, D.J. and Williams, T.A. Statistics for Business and Economics, 6th edition, West Publishing Company, 1996.Google Scholar
22. Hoerner, S.F. Fluid Dynamic Drag, Hoerner Fluid Dynmics, Brick Town, New Jersey, 1965.Google Scholar