Analysis of an Airdrop Motion Coupling N-S Equations with 6 DOF Motion Equations

Ping Hu; Li Xin Wang; Liang Min Guo

doi:10.4028/www.scientific.net/AMR.1016.506

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 1016Analysis of an Airdrop Motion Coupling N-S...

Analysis of an Airdrop Motion Coupling N-S Equations with 6 DOF Motion Equations

Abstract:

An airdrop model with aerial carrier is carried out to simulate an airdrop test. A coupled CFD/6 DOF is designed to compute the orientation and trajectory of the airdrop model. The results show that the CFD/6 DOF coupled method is appropriate to simulate this problem with a sufficient precision. The airdrop’s motion is strongly coupled with the aerodynamic force after leaving the sliding rail and the trajectory of its CG is mainly in the symmetry of the aerial carrier. The variation of its orientation mainly rolls in X axis direction and it swings as an approximate periodic oscillation which amplitude decreases over time. The maximum angle of orientation in X axis direction is-116°in 5 seconds. The similar variation of the airdrop motion is present in different angle of attack and sideslip of the aerial carrier.

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Periodical:

Advanced Materials Research (Volume 1016)

Pages:

506-510

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1016.506

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Online since:

August 2014

Authors:

Ping Hu*, Li Xin Wang, Liang Min Guo

Keywords:

Aerodynamic Performance, Airdrop Model, Computational Fluid Dynamics (CFD), Equation of Motion, N-S Equation

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References

[1] G. L. Winehenbach, G. T. Chapman etc. Dynamic Stability of Blunt Atmospheric Entry Configurations. Journal of spacecraft and rockets. 2002: 39(1): 51-55.

DOI: 10.2514/2.3781

Google Scholar

[2] F. M. Cheatwood, G. Chapman. Dynamic Stability Testing of the Genesis Sample Return Capsule. AIAA: 2000-1009; (2000).

DOI: 10.2514/6.2000-1009

Google Scholar

[3] G. T. Chapman, L. A. Yates. Limit Cycle Analysis of Blunt Entry Vehicles. AIAA: 99-1022; (1999).

Google Scholar

[4] R. A. Mitehcltree, S. Kellas, A Passive Search-Entry Capsule for Mars Sample Return. AIAA: 98-2851; (1998).

Google Scholar

[5] H. J. Hunter. Developmental airdrop testing techniques and devices [R]. AGARD-AG-300-Vol. 6.

Google Scholar

[6] B Bagdonovich, K. J. Desabrais, R. Benney etc. Overview of the Precision Airdrop Improvement Four-powers Long Term Technology Project [R]. AIAA 2003-2102.

DOI: 10.2514/6.2003-2102

Google Scholar

[7] Mark Mc Quilling and Jean Potvin. Simulation the Flows About Cargo Containers Used During Parachute Airdrop Operations . Journal of Aircraft. Vol. 48, No. 4, July-August (2011).

DOI: 10.2514/1.c031299

Google Scholar