The paper presents results of experimental investigations on flexible rectangular canopies fixed at two edges (tapes). Data are presented for the aerodynamic drag as a function of the planform area, the slenderness, and the Reynolds number. The slenderness varies from 3.3 to 30. The Reynolds number is limited to 2×106. The wind speed is in the range 619ms. The results show that the drag decreases with the increasing aspect ratio. The dominant parameter is the slenderness; a second dominant factor is the planform area. The drag is only weakly dependent on the Reynolds number. The analysis of the drag data indicates that a proper scaling parameter is the crosswise length scale. When normalization is done, the data tend to collapse into a single curve. A further study addressed the drag characteristics of the canopies with perforated planforms. Perforation of up to 6% of the planform area has been considered. Corrections for air permeability of the fabric are introduced. The drag is reduced roughly linearly with perforated area. A detailed study into the flutter characteristics of the canopies in the turbulent wind is presented. The investigation has highlighted different modes of oscillations, including deformations through folding and twisting, vertical flapping, rotations, and cross-type oscillations.

1.
Carruthers
,
A. C.
, 2005, “
Experimental Studies on the Drag and Flutter of Aerodynamic Decelerators
,” Ph.D. thesis, The University of Manchester, Manchester, UK.
2.
Carruthers
,
A. C.
, and
Filippone
,
A.
, 2005, “
The Aerodynamic Drag of Parafoils
,”
J. Aircr.
0021-8669,
42
(
4
), pp.
1081
1083
.
3.
Foreman
,
E. J.
, 1982, “
An Investigation Into the Performance of Sea Anchors for Inflatable Liferafts
,”
National Maritime Institute
, Technical Report No. NMI R-127.
4.
Matos
,
C.
,
Mahalingam
,
R.
,
Ottinger
,
G.
,
Klapper
,
J.
,
Funk
,
R.
, and
Komerath
,
N.
, 1998, “
Wind Tunnel Measurements of Parafoil Geometry and Aerodynamics
,” AIAA Paper No. 98-0606.
5.
Bearman
,
P.
, 1971, “
An Investigation of the Forces on Flat Plates Normal to a Turbulent Flow
,”
J. Fluid Mech.
0022-1120,
46
(
1
), pp.
177
198
.
6.
Hoerner
,
S. F.
, 1965,
Fluid Dynamic Drag
.
7.
Schubauer
,
G. B.
, and
Dryden
,
H. L.
, 1935, “
The Effect of Turbulence on the Drag of Flat Plates
,” NACA, Technical Report No. 546.
8.
ESDU, 1972, “
Fluid Forces and Moments on Flat Plates
,” ESDU, Technical Report No. 70015.
9.
Taylor
,
G. I.
, and
Davies
,
R. M.
, 1944, “
The Aerodynamics of Porous Sheets
,”
ARC R&M 2237, Republished in the Scientific Papers of Sir Geoffrey Ingram Tailor
, Vol.
III
(
45
), pp.
391
405
.
10.
Taylor
,
G. I.
, 1944, “
Air Resistance of a Flat Plate of Very Porous Material
,”
ARC R&M 2236, Republished in the Scientific Papers of Sir Geoffrey Ingram Tailor
, Vol.
III
(
43
), pp.
383
386
.
You do not currently have access to this content.