/Aircraft Cessna Cj-1 in climb stage, Climbing with angle of attack equal to 8º. Cj-1 has the following data Weight=2038.75 kg Wing area = 50 m² CDo = 0.018 Aircraft speed in climbing = 25m/s e = 0.75 p at 300 m = 0.909 And the variation of angle of attack with lift coefficient shown in figure. 1.8 Calculate 1.4 1.2 I. the thrust and power required for climbing to high 1.4 3000 m Climbing rate CL aspect ratio=7

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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/Aircraft Cessna Cj-1 in climb stage, Climbing with anglé of attack equal to 8°.
Cj-1 has the following data
Weight =2038.75 kg
Wing area =
50 m2
CDo = 0.018
aspect ratio =7
Aircraft speed in elimbing
25m/s
e = 0.75
p at 300, m = 0.909
And the variation of angle of attack with lift coefficient
1.3
shown in figure.
1.6
14
Calculate
. 12
I.
the thrust and power required for climbing to high
C
10-
3000 m
II.
Climbing rate
04
8 30
Angle of ata
Transcribed Image Text:/Aircraft Cessna Cj-1 in climb stage, Climbing with anglé of attack equal to 8°. Cj-1 has the following data Weight =2038.75 kg Wing area = 50 m2 CDo = 0.018 aspect ratio =7 Aircraft speed in elimbing 25m/s e = 0.75 p at 300, m = 0.909 And the variation of angle of attack with lift coefficient 1.3 shown in figure. 1.6 14 Calculate . 12 I. the thrust and power required for climbing to high C 10- 3000 m II. Climbing rate 04 8 30 Angle of ata
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