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NIFE Engines Exam Questions and Verified Detailed Answers | Graded A+

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NIFE Engines Exam Questions and Verified Detailed Answers | Graded A+ the potential of fluid molecules at rest. within a gas generator is simply called pressure - static pressure the kinetic energy of fluid molecules in motion. within a gas generator is simply called velocity - dynamic pressure sum of pressure (static pressure) and velocity (dynamic pressure) - Total Pressure air is considered to be a _______________ _________________ - compressible fluid Airflow is considered to be relatively __________________ __________________ at subsonic speeds - incompressible fluid Bernoulli states that any incompressible fluid passing through a convergent opening causes the velocity to _______________ and the pressure to _________________________. - increase, decrease Bernoulli also states any ________________ in velocity will cause a ________________ in pressure, and vice versa. - increase, decrease

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February 8, 2025
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NIFE Engines Exam Questions and
Verified Detailed Answers | Graded A+

the potential of fluid molecules at rest. within a gas generator is simply called

pressure - ✔✔static pressure

the kinetic energy of fluid molecules in motion. within a gas generator is simply

called velocity - ✔✔dynamic pressure

sum of pressure (static pressure) and velocity (dynamic pressure) - ✔✔Total

Pressure

air is considered to be a _______________ _________________ -

✔✔compressible fluid

Airflow is considered to be relatively __________________

__________________ at subsonic speeds - ✔✔incompressible fluid

Bernoulli states that any incompressible fluid passing through a convergent

opening causes the velocity to _______________ and the pressure to

_________________________. - ✔✔increase, decrease

Bernoulli also states any ________________ in velocity will cause a

________________ in pressure, and vice versa. - ✔✔increase, decrease



Page 1 of 51
©NINJANERD 2025/2026. YEAR PUBLISHED 2025.

,Bernoulli's also states, "as a subsonic (incompressible) fluid passes through a

divergent opening the velocity will ___________________ and the pressure will

_______________________ - ✔✔decrease, increase

as airflow approaches or reaches supersonic speeds, the airflow becomes more

______________ - ✔✔compressible

A convergent opening will cause supersonic (compressible) airflow velocity to

________________ and the pressure to __________________- - ✔✔decrease,

increase

A divergent opening causes supersonic (compressible) airflow velocity to

_________________ and the pressure to ____________________ - ✔✔increase,

decrease

nozzles always ______________ velocity and _________________ pressure -

✔✔increase, decrease

Supersonic or subsonic airflow determines the _______________ or

_________________ shape of the nozzles/diffusers - ✔✔convergent, divergent

diffusers always decrease ________________ velocity and

_____________________ pressure - ✔✔decrease, increase




Page 2 of 51
©NINJANERD 2025/2026. YEAR PUBLISHED 2025.

,Gas generators use nozzles/diffusers within to increase subsonic airflow to

______________ speeds, decrease supersonic airflow to _______________

speeds - ✔✔supersonic, subsonic

________________ ______________ produces the high energy airflow needed

to create thrust in a gas turbine engine - ✔✔gas generator

all gas generators will minimally include... - ✔✔compressor, combustion

chamber, turbine

gas turbine engines have a cycle of operation known as the _____________

_____________. - ✔✔brayton cycle

brayton cycle consists of four events which occur simultaneously - ✔✔Intake,

Compression, Combustion, Exhaust

________________ engines have an operation known as the otto cycle. otto

cycle consists of four events which occur sequentially - ✔✔reciprocating

in a gas turbine engine, the _____________ is at the front opening of the engine,

increases _____________ and decrease _____________ - ✔✔inlet, pressure,

velocity




Page 3 of 51
©NINJANERD 2025/2026. YEAR PUBLISHED 2025.

, in a gas turbine engine the _________________ comes right after the inlet to

increase velocity, temperature, pressure, total pressure (not ____________

system) - ✔✔compressor, closed

in a gas turbine engine, the ______________ is part of compressor and is used

to increase pressure, decrease velocity - ✔✔diffuser

in a gas turbine engine, the ______________ ________________ is where the

air/fuel is combusted, increase ______________ and ______________. slight

decrease in _______________ (gas turbine engine) - ✔✔combustion chamber,

temperature, velocity, pressure

in a gas turbine engine, the _________________ increases velocity, decrease

pressure. it use most kinetic energy to turn compressor - ✔✔turbine

in a gas turbine engine, the _________________ provides the final velocity

increase, pressure decrease - ✔✔exhaust

Thrust equation - ✔✔T = m x a

_______________ _____________ is measured on stationary engines or on

aircraft ground run-ups. based on standard day conditions (29.92, 15 degrees C).

ignores the velocity of air at the inlet and measures exhaust gas velocity only -

✔✔Gross thrust


Page 4 of 51
©NINJANERD 2025/2026. YEAR PUBLISHED 2025.

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