Skip to main content

Table 1 A summary of previous experimental studies on flow over inclined flat plate

From: Effects of aspect ratio and inclination angle on aerodynamic loads of a flat plate

Experiments

Aspect Ratio (AR)

Thickness/Chord

Reynolds (based on chord length and inlet velocity)

Inclination angle

Fage and Johansen [1]

14.1 (infinite)

0.03

150,000

0.15° ~ 90°

12° ~ 90°

Flaschbart [2]

50 ~ 200

0.015 ~ 0.05

1000 ~ 6000

90°

Schubauer and Dryden [3]

6

30,000 ~ 60,000

90°

Roshko [4]

13.5

0.16

4000 ~ 10,000

90°

Arie and Rouse [5]

12

0.083

75,000

90°

Fail, Lawford and Eyre [6]

1 ~ 20

80,000

90°

Abernathy [7]

1.5 ~ 6

0.06 ~ 0.19

36,000 ~ 140,000

40° ~ 90°

Castro [8]

15

0.04

25,000 ~ 90,000

90°

Sarpkaya & Kline [9]

8

0.11

21,000

90°

Kiya and Matsumura [10]

15

0.215

23,000

90°

Mazharoglu and Hacisevki [11]

14

0.2

33,000

90°

Xu et al. [12]

12.1

0.125

2240

90°