AMT 287 FINAL EXAM QUESTIONS WITH
CORRECT ANSWERS
who |first |developed |gas |turbine |type |accessory |for |aircraft |use |- |CORRECT |ANSWER✔✔-Moss
Aircraft |from |first |turbojet |propelled |flight |in |GB |- |CORRECT |ANSWER✔✔-Gloster |E-28/29
when |did |first |british |turbojet |flight |test |take |place |- |CORRECT |ANSWER✔✔-1941
who |developed |the |gas |turbine |engine |installed |in |the |HE-178, |which |was |the |first |successful |
prototype |turbojet |aircraft |- |CORRECT |ANSWER✔✔-Von |Ohain
what |company |developed |the |first |gas |turbine |engine |in |america |- |CORRECT |ANSWER✔✔-
General |Electric |Company
four |types |of |jet |engines |- |CORRECT |ANSWER✔✔-ROCKET |JET
PULSE |JET
RAM |JET
TURBO |JET
What |is |the |only |non |air |breathing |jet |engine |- |CORRECT |ANSWER✔✔-rocket |jet
what |are |the |four |types |of |aircraft |gas |turbine |engines |- |CORRECT |ANSWER✔✔-turboJET
turboFAN
turboPROP
, turboSHAFT
two |types |of |thrust |producing |engines |are |- |CORRECT |ANSWER✔✔-turboJET |and |turboFAN
two |types |of |torque |producing |engines |are |- |CORRECT |ANSWER✔✔-turboPROP |and |
turboSHAFT
the |two |turbine |design |classifications |of |turboprop |and |turboshaft |engines |are |- |CORRECT |
ANSWER✔✔-fixed |turbine |and |free |turbine
three |classifications |of |turboFAN |engines |are |- |CORRECT |ANSWER✔✔-low, |medium, |high |
bypass
if |a |hot |exhaust |of |a |gas |turbine |engine |produces |no |reactive |thrust, |what |type |of |engine |is |it
|- |CORRECT |ANSWER✔✔-turboSHAFT
high |bypass |turbofan |refers |to |what |significant |engine |ratio |- |CORRECT |ANSWER✔✔-fan |vs |
core |engine |MASS |AIRFLOW |ratio
mass |is |the |same |as |_______ |near |the |surface |of |the |earth |- |CORRECT |ANSWER✔✔-Weight
when |water |is |flowing |from |the |sprinkler |heads, |its |referred |to |as |_________ |energy |- |
CORRECT |ANSWER✔✔-kinetic
what |term |best |represents |potential |and |kinetic |energies |in |a |turbine |engine |- |CORRECT |
ANSWER✔✔-heat |and |motion |of |airflow
Bernoulli's |principal |refers |to |airflow |at |a |constant |value |(lbs/sec) |through |a |frictionless |duct |
and |at |a |________ |flow |rate |- |CORRECT |ANSWER✔✔-subsonic
CORRECT ANSWERS
who |first |developed |gas |turbine |type |accessory |for |aircraft |use |- |CORRECT |ANSWER✔✔-Moss
Aircraft |from |first |turbojet |propelled |flight |in |GB |- |CORRECT |ANSWER✔✔-Gloster |E-28/29
when |did |first |british |turbojet |flight |test |take |place |- |CORRECT |ANSWER✔✔-1941
who |developed |the |gas |turbine |engine |installed |in |the |HE-178, |which |was |the |first |successful |
prototype |turbojet |aircraft |- |CORRECT |ANSWER✔✔-Von |Ohain
what |company |developed |the |first |gas |turbine |engine |in |america |- |CORRECT |ANSWER✔✔-
General |Electric |Company
four |types |of |jet |engines |- |CORRECT |ANSWER✔✔-ROCKET |JET
PULSE |JET
RAM |JET
TURBO |JET
What |is |the |only |non |air |breathing |jet |engine |- |CORRECT |ANSWER✔✔-rocket |jet
what |are |the |four |types |of |aircraft |gas |turbine |engines |- |CORRECT |ANSWER✔✔-turboJET
turboFAN
turboPROP
, turboSHAFT
two |types |of |thrust |producing |engines |are |- |CORRECT |ANSWER✔✔-turboJET |and |turboFAN
two |types |of |torque |producing |engines |are |- |CORRECT |ANSWER✔✔-turboPROP |and |
turboSHAFT
the |two |turbine |design |classifications |of |turboprop |and |turboshaft |engines |are |- |CORRECT |
ANSWER✔✔-fixed |turbine |and |free |turbine
three |classifications |of |turboFAN |engines |are |- |CORRECT |ANSWER✔✔-low, |medium, |high |
bypass
if |a |hot |exhaust |of |a |gas |turbine |engine |produces |no |reactive |thrust, |what |type |of |engine |is |it
|- |CORRECT |ANSWER✔✔-turboSHAFT
high |bypass |turbofan |refers |to |what |significant |engine |ratio |- |CORRECT |ANSWER✔✔-fan |vs |
core |engine |MASS |AIRFLOW |ratio
mass |is |the |same |as |_______ |near |the |surface |of |the |earth |- |CORRECT |ANSWER✔✔-Weight
when |water |is |flowing |from |the |sprinkler |heads, |its |referred |to |as |_________ |energy |- |
CORRECT |ANSWER✔✔-kinetic
what |term |best |represents |potential |and |kinetic |energies |in |a |turbine |engine |- |CORRECT |
ANSWER✔✔-heat |and |motion |of |airflow
Bernoulli's |principal |refers |to |airflow |at |a |constant |value |(lbs/sec) |through |a |frictionless |duct |
and |at |a |________ |flow |rate |- |CORRECT |ANSWER✔✔-subsonic
