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Miscellany

A vortex code for flow over rigid or flexible bluff bodies

Article: N42 | Received 03 Oct 2002, Published online: 24 Jan 2011

References

References

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  • Behr V L Wolfe W P Peterson C W Hailey C E 1999 An overview of the development of a vortex based inflation code for parachute simulation (VIPAR) 15th CEAS/AIAA Aerodynamic Decelerator Systems Technology Conf. (Toulouse, France, June 1999) (AIAA Paper 99–1726 (A99-30980))
  • Strickland J H 1993 A prediction method for unsteady axisymmetric flow over parachutes 12th RAeS/AIAA Aerodynamic Decelerator Systems Technology Conf. (London, UK, May 1993) (AIAA Paper 93-1217)
  • Strickland , J H . 1994 . AIAA J. Aircraft , 31 : 637 – 43 .
  • Sundberg W D 1999 PRONTO2D/VPARA coupling Internal Sandia National Laboratories Memorandum to W P Wolfe
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  • Strickland , J H , Gritzo , L A , Baty , R S , Homicz , G F and Burns , S P . 1999 . Fast multipole solvers for three-dimensional radiation and fluid flow problems . ESAIM Proc. , 7 : 408 – 17 .
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  • Gharakhani A 2000 A higher order vorticity redistribution method for 3-D diffusion in free space Sandia National Laboratory Report SAND2000-2505
  • Taylor L M Flanagan D P 1989 PRONTO3D, a three-dimensional transient solid dynamics program Sandia National Laboratory Report SAND87-1912
  • Ewing E G Bixby H W Knake T W 1978 Recovery system design guide Air Force Flight Dynamics Laboratory Technical Report AFFDL-TR-78-151

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