個班西HR 一年先請幾個 係度話candidate 唔夠班
嗰班on9 HR
個recruitment head係西中之西
過唔到 1B HR interview, 任你technical曉飛都無用
個班西HR 一年先請幾個 係度話candidate 唔夠班
嗰班on9 HR
個recruitment head係西中之西
嗰班on9 HR
個recruitment head係西中之西
過唔到 1B HR interview, 任你technical曉飛都無用
個recruitment head係西中之西
過唔到 1B HR interview, 任你technical曉飛都無用
1B 算易,panel in 先harsh
過唔到 1B HR interview, 任你technical曉飛都無用
1B 算易,panel in 先harsh
聽過有時HR都係隨便問兩句然後八成時間畀capt./SFO問tech
冇physics同數底
都幾難睇得明本野
下下睇兩睇就要google
冇physics同數底
都幾難睇得明本野
下下睇兩睇就要google
FAA? 其實本野寫得麻麻
2.其實係想compare raked wingtip vs conventional winglet
一個more efficient during cruising 一個more efficient on climbing
所以用係extra long haul vs mid long haul
2.其實係想compare raked wingtip vs conventional winglet
一個more efficient during cruising 一個more efficient on climbing
所以用係extra long haul vs mid long haul
Morning
Blended winglet (744)
1. Higher pressure in the outside face of the winglet
2. Lower pressure in the inside face of the winglet
3. Lift is generated
4. Forward lift component can be generated
5. More effective when high aoa as the pressure diff is higher
Raked wingtip (77w)
1. Higher AR, less drag
2. They kind of re-distributed the wingload, no solid ans for this one from me
Try try this:
" in steady climb, the lift is smaller, greater or equal to the weight? "
冇physics同數底
都幾難睇得明本野
下下睇兩睇就要google
FAA? 其實本野寫得麻麻
2.其實係想compare raked wingtip vs conventional winglet
一個more efficient during cruising 一個more efficient on climbing
所以用係extra long haul vs mid long haul
Morning
Blended winglet (744)
1. Higher pressure in the outside face of the winglet
2. Lower pressure in the inside face of the winglet
3. Lift is generated
4. Forward lift component can be generated
5. More effective when high aoa as the pressure diff is higher
Raked wingtip (77w)
1. Higher AR, less drag
2. They kind of re-distributed the wingload, no solid ans for this one from me
Try try this:
" in steady climb, the lift is smaller, greater or equal to the weight? "
Smaller 好易中伏
Morning
Blended winglet (744)
1. Higher pressure in the outside face of the winglet
2. Lower pressure in the inside face of the winglet
3. Lift is generated
4. Forward lift component can be generated
5. More effective when high aoa as the pressure diff is higher
Raked wingtip (77w)
1. Higher AR, less drag
2. They kind of re-distributed the wingload, no solid ans for this one from me
Try try this:
" in steady climb, the lift is smaller, greater or equal to the weight? "
Smaller 好易中伏
呢個堅伏 你又搵 d 問題吹下
Smaller 好易中伏
呢個堅伏 你又搵 d 問題吹下
就問下你個名啦 點解design要dihedral
呢個堅伏 你又搵 d 問題吹下
就問下你個名啦 點解design要dihedral
Increase lateral stability
冇physics同數底
都幾難睇得明本野
下下睇兩睇就要google
FAA? 其實本野寫得麻麻
真係,有 d 位有時寫到好虛
D 字又太 academic
但有時都 helpful 既
FAA? 其實本野寫得麻麻
真係,有 d 位有時寫到好虛
D 字又太 academic
但有時都 helpful 既
BAK應該比較好,深入淺出,但好似要上網訂實體書。
FAA嗰本可以用三版解釋一個concept,有一半以上係廢話,好處係唔洗錢
真係,有 d 位有時寫到好虛
D 字又太 academic
但有時都 helpful 既
BAK應該比較好,深入淺出,但好似要上網訂實體書。
FAA嗰本可以用三版解釋一個concept,有一半以上係廢話,好處係唔洗錢
Cx 而加1A用FAA 出mc
BAK應該比較好,深入淺出,但好似要上網訂實體書。
FAA嗰本可以用三版解釋一個concept,有一半以上係廢話,好處係唔洗錢
Cx 而加1A用FAA 出mc
咁FAA會好過佢自己本jki
FAA? 其實本野寫得麻麻
真係,有 d 位有時寫到好虛
D 字又太 academic
但有時都 helpful 既
BAK應該比較好,深入淺出,但好似要上網訂實體書。
FAA嗰本可以用三版解釋一個concept,有一半以上係廢話,好處係唔洗錢