Wind Tunnel Investigation of a Rigid Paraglider Reference Wing-Reference-Cited by-同舟云学术

Wind Tunnel Investigation of a Rigid Paraglider Reference Wing

Published:2015-03 Issue:2 Volume:52 Page:703-708
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Belloc H.¹

Affiliation:

1. Universite de Toulouse/ISAE, BP 54032-31055 Toulouse Cedex 4, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032513

Reference10 articles.

1. HassellJ. L.Jr.WareG. M. “Wind-Tunnel Investigation of Ram-Air-Inflated All-Flexible Wings of Aspect Ratios 1.0 to 3.0,” NASA TM-SX-1923, Dec. 1969.

2. NicolaidesJ. D. “Parafoil Wind Tunnel Tests,” Univ. of Notre Dame, Technical Rept. AFFDL TR-70-146, June 1971, DTIC: AD0731564.

3. GeigerR. H.WailesW. K. “Advanced Recovery Systems Wind Tunnel Test Report,” NASA Contractor Rept. 177563, Aug. 1990.

4. Large gliding parachute experimental and theoretical approaches

5. Wind tunnel measurements of parafoil geometry and aerodynamics

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