Computational aerodynamic modeling for flight dynamics simulation of ram-air parachutes-Reference-Cited by-同舟云学术

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Computational aerodynamic modeling for flight dynamics simulation of ram-air parachutes

Published:2016-07 Issue: Volume:54 Page:286-301
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ghoreyshi Mehdi,Bergeron Keith,Jirásek Adam,Seidel Jürgen,Lofthouse Andrew J.,Cummings Russell M.

Funder

USAFA

Department of Defense High Performance Computing Modernization Program

NSRDEC Airdrop Technology Team and the High Performance Computing Research Center at USAFA

US Air Force Academy

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. D.C. Jalbert, Multi-cell wing type aerial device, U.S. Patent No. 3,285,246.

2. The Parachute Manual: A Technical Treatise on Aerodynamic Decelerators, vol. 1;Poynter,1991

3. United States Government, US Federal Aviation Regulations, July 2012.

4. A review of para-foil applications;Nicolaides;J. Aircr.,1970

5. Parallel finite element simulation of large ram-air parachutes;Karlo;Int. J. Numer. Methods Fluids,1997

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