An overview of the development of a vortex based inflation code for parachute simulation (VIPAR)

15th Aerodynamic Decelerator Systems Technology Conference

Volumn , Issue , 1999, Pages

  Behr, Vance L ^a   Wolfe, Walter P ^a   Peterson, Carl W ^a   Hailey, Christine E ^b  

^a SANDIA NATIONAL LABORATORIES   (United States)

^b UTAH STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AGING OF MATERIALS; NUCLEAR WEAPONS;

CODE DEVELOPMENT; CURRENT STATUS; EXPERIENCE BASE; EXPERIENCED STAFF; EXPERIMENTAL VALIDATIONS; PARACHUTE SYSTEM; SANDIA NATIONAL LABORATORIES; TOOLS AND TECHNIQUES;

PARACHUTES;

EID: 84983157169     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-1726     Document Type: Conference Paper

References (17)

1. th AIAA Aerodynamic Decelerator Systems Technology Conference, June 3-5, 1997, San Francisco, CA.
2. Strickland, J. H., and H. Higuchi, "Parachute Aerodynamics: An Assessment of Prediction Capability," J. Aircraft, Vol. 33, No. 2, March-April 1996, pp 241-252.
3. Peterson, C. W., J. H. Strickland, and H. Higuchi, "The Fluid Dynamics of Parachute Inflation," Annu. Rev. FluidMech., Vol. 28, 1996, pp. 361-87.
4. rd Int. Workshop on Vortex Flows and Related Numerical Methods, Toulouse, FR, August, 1998, to be published in ESAIM Proceedings.
5. Gharakhani, A., "A Survey of Grid-Free Methods for the Simulation of 3-D Incompressible Flows in Bounded Domains," SAND 97-2256, Sandia National Laboratories, NM, September 1997.
6. Batchelor, G. K., An Introduction to Fluid Dynamics. Sec. 5.2, Cambridge University Press, Cambridge, 1967.
7. Currie, I. G., Fundemental Mechanics of Fluids. Section 3.4, McGraw Hill, Inc. 1974.
8. Homicz, G. F., "FY98 ESRF Effort on Gridless Methods for Compressible Flows," internal memorandum, Sandia National Laboratories, Albuquerque, New Mexico, October, 14, 1998.
9. Clarke, N. R. and O. R. Tutty, "Construction and Validation of a Discrete Vortex Method for the Two-Dimensional Incompressible Navier-Stokes Equations," Computers and Fluids, Vol. 23, No. 6, pp. 751-783, 1994.
10. Attaway, S. W., et al., "PR0NT03D User's Instructions: A Transient Dynamic Code for Nonlinear Structural Analysis," SAND98-1361, Sandia National Laboratories, Albuquerque, NM,' June 1998.
11. Blacker, T. D., et al., "CUBIT Mesh Generation Environment, Volume 1: Users Manual," SAND94-1100, Sandia National Laboratories, Albuquerque, NM, May 1994.
12. "PR0NT02D/VPARA Coupling." Internal Memorandum from W. D. Sundberg to W. P, Wolfe, Sandia National Laboratories, Albuquerque, NM, 11 Jan., 1999.
13. th CEAS/AIAA Aerodynamic Decelerator Systems Technology Conference, Toulouse, FR, 9-11 June, 1999.
14. th Int. Congress on Instrumentation in Aerospace Simulation Facilities, Toulouse, FR, 14-17 June, 1999.
15. "External Program Review of VIPAR: comments from the March 29, 1999 Meeting," submitted to the VIPAR Program, Sandia National Laboratories, April 30, 1999.
16. Strickland, J. H. and R. S. Baty, "A Pragmatic Overview of Fast Multipole Methods," Lectures in App. Math., Vol. 32, 1996.
17. Strickland, J. H., "Axisymmetric Bluff-Body Flow: A Vortex Solver For Thin Shells," SAND91-2760, Sandia National Laboratories, Albuquerque, NM, May, 1992.