Development of a massively parallel parachute performance prediction code-Reference-Cited by-同舟云学术

Development of a massively parallel parachute performance prediction code

Published:1997-06-03 Issue: Volume: Page:
ISSN:
Container-title:14th Aerodynamic Decelerator Systems Technology Conference
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Author:

Peterson Carl¹,Strickland James¹,Wolfe Walter¹,Sundberg W.¹,McBride Donald¹,Peterson Carl¹,Strickland James¹,Wolfe Walter¹,Sundberg W.¹,McBride Donald¹

Affiliation:

1. Sandia National Labs., Albuquerque, NM

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1504

Reference17 articles.

1. Parachute aerodynamics - An assessment of prediction capability (1995)

2. Computational fluid dynamic studies of a solid and ribbon 12-gore parachute canopy in subsonic and supersonic flow

3. Stein, K. R.,Benney,R. J., and Steeves, E. C. "A Computational Model That Couples Aerodynamic and Structural Dynamic Behavior of ParachutesDuringtheOpeningProcess,"U.S. Army Technical Report NATICK/TR-93/029, February 1993.

4. Stein, K. R. and Benney, R. J. "Parachute Inflation: A Problem in Aeroelasticity," U. S. Army Technical Report NATICK/TR-94/015, February, 1994.

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1. On the development of a gridless inflation code for parachute simulations;16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2001-05-21

2. Simple Description of Airflow Characteristics Inside an Unfolding Parachute;Journal of Aircraft;1999-09

3. An overview of the development of a Vortex Based Inflation Code for Parachute Simulation (VIPAR);15th Aerodynamic Decelerator Systems Technology Conference;1999-06-08