What thrust is obtained from a propeller 3 m in diameter that has the characteristics given in Fig. 14.2 when the propeller is operated at an angular speed of 1400 rpm and an advance velocity of zero? Assume p = 1.05 kg/m³. Figure 14.2 0.06 60 Dimensionless performance curves for a typical propeller; D = 2.90 m. n = 1400 0.05 50 rpm. [After Weick (1).] 0.04 40 0.03 Ст 30 0.02 20 CP 0.01 10 0.1 0.2 0.3 0.4 0.5 C, and C, Efficiency, percent

Elements Of Electromagnetics
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2. What thrust is obtained from a propeller 3 m in diameter that has the characteristics given in Fig. 14.2
when the propeller is operated at an angular speed of 1400 rpm and an advance velocity of zero?
Assume p = 1.05 kg/m³.
Figure 14.2
0.06
60
Dimensionless
performance curves for a
0.05
50
typical propeller;
D = 2.90 m, n = 1400
rpm. [After Weick (1).]
0.04
40
0.03-
CT
30
0.02E
20
Cp
0.01
10
0.1
0.2
0.3
0.4
0.5
Vo
nD
Cp and C-
Efficiency, percent
Transcribed Image Text:2. What thrust is obtained from a propeller 3 m in diameter that has the characteristics given in Fig. 14.2 when the propeller is operated at an angular speed of 1400 rpm and an advance velocity of zero? Assume p = 1.05 kg/m³. Figure 14.2 0.06 60 Dimensionless performance curves for a 0.05 50 typical propeller; D = 2.90 m, n = 1400 rpm. [After Weick (1).] 0.04 40 0.03- CT 30 0.02E 20 Cp 0.01 10 0.1 0.2 0.3 0.4 0.5 Vo nD Cp and C- Efficiency, percent
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