14th Aerodynamic Decelerator Systems Technology Conference 1997
DOI: 10.2514/6.1997-1482
|View full text |Cite
|
Sign up to set email alerts
|

Large gliding parachute experimental and theoretical approaches

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2004
2004
2017
2017

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(1 citation statement)
references
References 0 publications
0
1
0
Order By: Relevance
“…Experimental investigations (Burk and Ware, 1967;Nicolaides et al, 1970;Ware and Hassell, 1969;Tribot et al, 1997), have established that the leading edge air inlet has a significant impact on the flow characteristics and thus the performance of a parafoil. These findings have been reproduced numerically by two-and three-dimensional potential flow computations performed by Ross (1993).…”
Section: Introductionmentioning
confidence: 99%
“…Experimental investigations (Burk and Ware, 1967;Nicolaides et al, 1970;Ware and Hassell, 1969;Tribot et al, 1997), have established that the leading edge air inlet has a significant impact on the flow characteristics and thus the performance of a parafoil. These findings have been reproduced numerically by two-and three-dimensional potential flow computations performed by Ross (1993).…”
Section: Introductionmentioning
confidence: 99%