ATP CTP FINAL EXAM NEWEST 2024 ACTUAL EXAM COMPLETE QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS) GET IT 100% RIGHT!!
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Course
ATP CTP
Institution
ATP CTP
ATP CTP FINAL EXAM NEWEST 2024
ACTUAL EXAM COMPLETE QUESTIONS
AND CORRECT DETAILED ANSWERS
(VERIFIED ANSWERS) GET IT 100% RIGHT!!
ATP CTP FINAL EXAM NEWEST 2024
ACTUAL EXAM COMPLETE QUESTIONS
AND CORRECT DETAILED ANSWERS
(VERIFIED ANSWERS) GET IT 100% RIGHT!!
ATP CTP FINAL EXAM NE...
ATP CTP FINAL EXAM NEWEST 2024
ACTUAL EXAM COMPLETE QUESTIONS
AND CORRECT DETAILED ANSWERS
(VERIFIED ANSWERS) GET IT 100% RIGHT!!
Which of the following statements regarding energy is true?
(A) Kinetic energy decreases
with increasing airspeed.
(B) Potential energy is approximately
proportional to airspeed.
(C) Chemical energy remains
constant throughout a flight
(D) Kinetic energy can be traded for potential energy, and
potential energy can be traded for kinetic energy -
ANSWER-(D) Kinetic energy can be traded for potential energy, and
potential energy can be traded for kinetic energy
The objective in maneuvering the airplane is to manage energy so
that:
(A) Kinetic energy stays between limits (stall and placard)
(B) Potential energy sstays between limits (terrain and buffet altitude)
,(C) Chemical energy stays above certain thresholds (not running out of
fuel) (D) All of the above - ANSWER-(D) All of the above
What is the effect on total drag is airspeed slows below L/D Max?
(A) Drag increases because of increased parasite drag
(B) Drag decreases because of lower induced drag
(C) Drag increases because of increased induced drag - ANSWER-(C)
Drag increses because of increased induced drag
A jet pilot flying at L/D Max is obtain best:
(A)
Range
(B)
Endurance
(C) Ride Quality -
ANSWER-(B) Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum
range, which type of drag predominates?
(A)
Parasite
(B)
Induced
,(C) Each type of drag contributes
equally - ANSWER-(A) Parasite
While already at high speed, what happens if Mach is allowed to
increase?
(A) Airflow over parts of the airplane begin
to exceed the speed of sound
(B) Shock waves can cause
local airflow separation
(C) Characteristics such as pitch-up, pitch-
down, or buffeting may occur.
(D) All of the above - ANSWER-
(D) All of the above
What is the result of a shock-induced separation of airflow occurring
symmetrically near the wing root of a swept wing
aircraft?
(A) A high-speed stall and
sudden pitch-up
(B) Severe
porpoising.
(C) A severe moment or "Mach Tuck - ANSWER-(C) A severe moment
or "Mach Tuck
, The speed of sound generally decreases with increasing altitude. This
occurs because:
(A) The air
temperature
decreases.
(B) The air
pressure
decreases.
(C) The composition of the air changes. - ANSWER-
(A) The air temperature decreases.
Critical Mach number can be defined as:
(A) The speed at which the aircraft is traveling faster than sound.
(B) The maximum Mach number at which an aircraft may be safely
operated.
(C) The speed of an aicraft in which airflow over any part of the aircraft
or structure first reaches, but doesn't exceed, Mach 1.0. - ANSWER-
(C) The speed of an aicraft in which airflow over any part of the
aircraft or structure first reaches, but doesn't exceed, Mach 1.0.
Stability in the vertical axis tends to drive the sideslip angle toward
zero. The most dynamic stability about the vertical
axis on modern jet
transports is from:
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