Simulation of Flowfield Around a Ram-Air Personnel Parachute Canopy-Reference-Cited by-同舟云学术

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Simulation of Flowfield Around a Ram-Air Personnel Parachute Canopy

Published:2013-09 Issue:5 Volume:50 Page:1628-1636
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Eslambolchi A.¹,Johari H.¹

Affiliation:

1. Mechanical Engineering Department, California State University, Northridge, California 91330

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032169

Reference14 articles.

1. BurkS. M.WareG. M. “Static Aerodynamic Characteristics of Three Ram-Air Inflated Low Aspect Ratio Wings,” NASA TN-D-4182, 1967.

2. A review of para-foil applications

3. WareG. M.HassellJ. L. “Wind Tunnel Investigations of Ram-Air Inflated All-Flexible Wings of Aspect Ratio 1.0 to 3.0,” NASA TM-SX-1923, 1969.

4. Large gliding parachute experimental and theoretical approaches

5. RossJ. C. “Computational Aerodynamics in the Design and Analysis of Ram-Air-Inflated Wings,” AIAA Paper 93-1228, May 1993.

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