A prediction method for unsteady axisymmetric flow over parachutes

AIAA/AHS/ASEE Aerospace Design Conference, 1993

Volumn , Issue , 1993, Pages

  Strickland, J H ^a  

^a SANDIA NATIONAL LABORATORIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; SPHERES; VORTEX FLOW; VORTICITY;

ARBITRARY VELOCITIES; COMPUTER PROCESSING; DIRECT CALCULATION; FAST MULTIPLE METHOD; PREDICTION METHODS; SOLUTION TECHNIQUES; UNSTEADY AXISYMMETRIC FLOW; VORTICITY TRANSPORT EQUATIONS;

BODIES OF REVOLUTION;

EID: 85006256559     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (45)

1. Macha, J. M., “An Introduction to Testing Parachutes in Wind Tunnels,” AIAA Paper No. 91-0858, AIAA 11th Aerodynamic Dccelerator Systems Technology Conference, San Diego, California, April 1991.
2. Clements, R. R. and Maul I D. J., “The Representation of Sheets of Vorticity by Discrete Vortices,” Progress in Aerospace Sciences, vol. 16, p. 129, 1975.
3. Sarpkaya, T “Computational Methods With Vortices,” Journal of Fluids Engineering, vol. 111, no. 1, March 1989.
4. Saffman, P. G. and Baker, G. R., “Vortex Interactions,” Annual Review of Fluid Mechanics, vol. 11, pp. 95-122, 1979.
5. Leonard, A., “Vortex Methods for Flow Simulation,” Journal of Computational Physics, vol. 37, pp. 289-335, 1980.
6. de Bemardinis, B., Graham, J. M. R., and Parker, K. H., “Oscillatory Flow Around Disks and Through Orifices,” Journal of Fluid Mechanics, vol. 102, pp. 279-299, 1981.
7. Kiya, M., Sasaki, K., and Arie, M., “Discrete Vortex Simulation of a Separation Bubble,” Journal of Fluid Mechanics, vol. 120, pp. 219-244, 1982.
8. Kiya, M. and Arie, M., “A Contribution to an Inviscid Vortex Shedding Model for an Inclined Flat Plate in Uniform Flow,” Journal of Fluid Mechanics, vol. 82, pp. 223-240, 1977.
9. Sarpkaya, T., “An Inviscid Model of 2-Dimen-sional Vortex Shedding for Transient and Asymptotically Steady Separated Flow Over an Inclined Flat Plate,” Journal of Fluid Mechanics, vol. 68, pp. 109-128, 1975.
10. Sarpkaya, T. and Schoaff, R. L., “Inviscid Model of 2-Dimensional Vortex Shedding by a Circular Cylinder,” AIAA Journal, vol. 17, no. 11, pp. 1193-1200, 1979.
11. Sarpkaya, T. and Kline, H. K., “Impulsively Started Flow About Four Types of Bluff Body,” Journal of Fluids Engineering, vol. 104, pp. 207-213, 1982.
12. Katz, J., “A Discrete Vortex Method for the Non-Steady Separated Flow Over an Airfoil.” Journal of Fluid Mechanics, vol. 102, pp. 315-328, 1981.
13. Spalart, P. R. and Leonard, A., “Computation of Separated Rows by a Vortex Tracing Algorithm,” AIAA Paper No. 81-1246, AIAA 14th Fluid and Plasma Dynamics Conference, Palo Alto, California, June 1981.
14. Im B. J., Oler, J. W., Strickland, J. H., MA Coupled Viscid-Inviscid Calculation Method for the Prediction of Unsteady Separated Rows Over an Airfoil,” AIAA Paper No. 88-0566, AIAA 26th Aerospace Science Meeting, Reno, Nevada, January 1988.
15. Spalart, P. R., “Vortex Methods for Separated Flows,” NASA-TM-100068, June 1988.
16. Stansby, P. K “A Generalized Discrete Vortex Method for Sharp-Edged Cylinders,” AIAA Journal, vol. 23, pp. 856-861, 1985.
17. Smith, P. A., and Stansby, P. K., “Impulsively Started Flow Around a Circular Cylinder by the Vortex Method,” Journal of Fluid Mechanics, vol. 194, pp. 45-77, 1988.
18. Rcbbach, C., “Numerical Calculation of Three-Dimensional Unsteady Flows with Vortex Sheets,” AIAA Paper No. 78-111, AIAA 16th Aerospace Sciences Meeting, Huntsville, Alabama, January 1978.
19. Sarpkaya, T., “Unsteady Flow about Porous Cambered Shells,” Journal of Aircraft, Vol. 28, No. 8, pp. 502-508, August 1991.
20. Klimas, P. C., ‘Fluid Mass Associated with an Axisymmetric Parachute Canopy,” Journal of Aircraft, vol. 14, pp. 577-580, 1977.
21. Ibrahim, S. K, “Potential Flow Field and Added Mass of the Idealized Hemispherical Parachute,” Journal of Aircraft, vol. 4, pp. 96-100, 1967.
22. Roberts, B. W., “Aerodynamic Inflation of Shell Type, Parachute Structures,” Journal of Aircraft, vol. 11, pp. 390-396, 1974
23. Sarpkaya, T., Mostafa, S. M. and Munz, P. D., “Numerical Simulation of Unsteady Flow about Cambered Plates,” Journal of Aircraft, Vol. 27, No. 1, pp. 51-59, January 1990.
24. Oler, J. W., Lawrence, J. H., and Adamson, T. D., “Unsteady Loads on Rigid Two-Dimen-sional Parachutes,” Sandia National Laboratories Report SAND88-7024, August 1990.
25. Strickland, J. H., “A Vortex Panel Analysis of Circular-Arc Bluff Bodies In Unsteady Flow,” AIAA Paper No. 89-0930, AIAA 10th Aerodynamic Decelerator Systems Technology Conference, Cocoa Beach, Florida, April 1989.
26. Higuchi, H. and Park, W. C. “Computations of the Flow Past Solid and Slotted Two-Dimensional Bluff Bodies with Vortex Tracing Method,” AIAA Paper No. 89-0929, AIAA 10th Aerodynamic Decelerator Systems Technology Conference, Cocoa Beach, Florida, April 1989.
27. Ashurst, W. T., “Application of Lagrangian Vortex Dynamics to Parachute Flow Fields,” Internal Communications, Sandia National Laboratories.
28. McCoy, H. H. and Werme, T. D., “Axisyinmct-ric Vortex Lattice Method Applied to Parachute Shapes,” AIAA Paper No. 86-2456, 1986.
29. Shirayama, S. and Kuwahara, K., “Computation of Flow Past a Parachute by a Three-Dimensional Vortex Method,” AIAA Paper No. 86-0350, AIAA 24th Aerospace Sciences Meeting, Reno, Nevada, January 1986.
30. Frucht, Y., and Cockrell, D., “A Discrete Vortex Method of Analysis for Inviscid Axisymmetric Flows Around Parachute Canopies.” AIAA Paper No. 91-0850, AIAA 11th Aerodynamic Decelerator Systems Technology Conference, San Diego, California, April 1991.
31. Koo, J. K., and James, D. F., “Fluid Flow Around and Through a Screen,” J. Fluid Mech., vol. 60, pp. 513-538, 1973.
32. Taylor, G. I., and Batchelor, G. K., “The Effect of Wire Gauze on Small Disturbances in a Uniform Stream,” Quart. Joum. Mech and Applied Math., vol. 2, Pt. I, pp. 1-29, 1949.
33. Currie, I. G., Fundamental Mechanics of Fluids, McGraw-Hill, p. 46, 1974.
34. Ogami, Y., and Akamatsu, T., “Viscous Flow Simulation Using the Discrete Vortex Model -The Diffusion Velocity Method,” Computers & Fluids, vol. 19, no. 3/4, pp. 433-441, 1991.
35. Chapra, S. C., and Canale, R. P., “Numerical Methods For Engineers With Personal Computer Applications,” p. 526, McGraw-Hill, 1985.
36. Strickland, J. H., and Amos, D. E., “Fast Solver for Systems of Axisymmetric Ring Vortices,” AIAA Journal, Vol.30, No. 3, pp. 737-746, March, 1992.
37. Carrier, J., Greengard, L., and Rokhlin, V., “A Fast Adaptive Multipole Algorithm For Particle Simulations,” SIAM Journal on Scientific and Statistical Computing, vol. 9, no. 4, pp. 669-686, July 1988.
38. Strickland, J. H., “Axisymmetric Bluff-Body Flow: A Vortex Solver For Thin Shells,” Sandia National Laboratory Report SAND91-2760,64 pages, May 1992.
39. Hoemer, S. F.f Fluid-Dynamic Drag, published by the author, pp. 3-16, 1965.
40. Beannan, P. W., and Takamoto, M., “Vortex Shedding Behind Rings and Disks,” Fluid Dynamics Research, Vol. 3, pp. 214-218, 1988.
41. Higuchi, H., “Wake Behind a Circular Disk in Unsteady and Steady Incoming Streams,” AIAA paper No. 91-0852, AIAA 11th Aerodynamic Decelerator Systems Technology Conference, San Diego, California, April 1991.
42. White, F. M., Fluid Mechanics, McGraw-Hill, New York, p. 436, 1979.
43. Oler, J. W., Unpublished data to be included in final contract report, 1992
44. Lamb, H., Hydrodynamics, 6th ed., Dover Publications, New York, pp. 236-241, 1945
45. Sadowsky, M. A. and Sternberg, E., “Elliptic Integral Representation of Axially Symmetric Rows,” Quarterly of Applied Mathematics, vol. 8, pp. 113-126, July 1950.