問題一覧
1
clear exhaust from the airframe
2
to shield turbine disc rear face and slow gases velocity
3
optimize thrust at the outlet from the engine.
4
pressure thrust.
5
the basic form and the earliest type of turbojet engine
6
accelerate the airflow from the turbine to make thrust
7
at the last stage of the turbine
8
reduce noise, by induce cooled air to mix with hot gases.
9
slow down aircraft speed on ground
10
less than max due to structural limits (low power and low forward speed)
11
the turbine
12
pure jet and low by pass engine
13
to prevent inadvertent operation of thrust reversal in commercial air transport
14
gas flow is mach1 at the exit
15
to provide braking and directional control during emergency landings back an aircraft out of a parking spot "power back"
mod5 training
mod5 training
ユーザ名非公開 · 14問 · 1年前mod5 training
mod5 training
14問 • 1年前M6c1
M6c1
ユーザ名非公開 · 22問 · 1年前M6c1
M6c1
22問 • 1年前M6c2
M6c2
ユーザ名非公開 · 20問 · 1年前M6c2
M6c2
20問 • 1年前M6c3
M6c3
ユーザ名非公開 · 52問 · 1年前M6c3
M6c3
52問 • 1年前M6c4
M6c4
ユーザ名非公開 · 26問 · 1年前M6c4
M6c4
26問 • 1年前M6c5
M6c5
ユーザ名非公開 · 48問 · 1年前M6c5
M6c5
48問 • 1年前M6c6
M6c6
ユーザ名非公開 · 27問 · 1年前M6c6
M6c6
27問 • 1年前M6c7
M6c7
ユーザ名非公開 · 15問 · 1年前M6c7
M6c7
15問 • 1年前M6c8
M6c8
ユーザ名非公開 · 15問 · 1年前M6c8
M6c8
15問 • 1年前M6c9
M6c9
ユーザ名非公開 · 17問 · 1年前M6c9
M6c9
17問 • 1年前M6c10
M6c10
ユーザ名非公開 · 18問 · 1年前M6c10
M6c10
18問 • 1年前M6c11
M6c11
ユーザ名非公開 · 44問 · 1年前M6c11
M6c11
44問 • 1年前M7c1
M7c1
ユーザ名非公開 · 18問 · 1年前M7c1
M7c1
18問 • 1年前M7c2
M7c2
ユーザ名非公開 · 11問 · 1年前M7c2
M7c2
11問 • 1年前M7c3
M7c3
ユーザ名非公開 · 39問 · 1年前M7c3
M7c3
39問 • 1年前M7c4
M7c4
ユーザ名非公開 · 21問 · 1年前M7c4
M7c4
21問 • 1年前M10c1
M10c1
ユーザ名非公開 · 15問 · 1年前M10c1
M10c1
15問 • 1年前M7c5
M7c5
ユーザ名非公開 · 11問 · 1年前M7c5
M7c5
11問 • 1年前問題一覧
1
clear exhaust from the airframe
2
to shield turbine disc rear face and slow gases velocity
3
optimize thrust at the outlet from the engine.
4
pressure thrust.
5
the basic form and the earliest type of turbojet engine
6
accelerate the airflow from the turbine to make thrust
7
at the last stage of the turbine
8
reduce noise, by induce cooled air to mix with hot gases.
9
slow down aircraft speed on ground
10
less than max due to structural limits (low power and low forward speed)
11
the turbine
12
pure jet and low by pass engine
13
to prevent inadvertent operation of thrust reversal in commercial air transport
14
gas flow is mach1 at the exit
15
to provide braking and directional control during emergency landings back an aircraft out of a parking spot "power back"