AVIA 305 Final Exam Review 2025 |
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Terms in this set (131)
Aerodynamic Lift and Drag
Force (AF)
resolves into
which two
aerodynamic
components?
,The aerodynamic Lift
component that
is 90 ° to the
flight path and
acts toward the
top of the
airplane is
called:
The aerodynamic Drag
component that
is parallel to the
flight path and
acts toward the
rear of the
airplane is
called:
The measure of Mass
the amount of
material
contained in a
body is called:
,The force Weight
influenced by
the gravitational
attraction of the
earth, moon, or
sun is called:
Equilibrium is - There must be no unbalanced
defined as "a forces acting on the body.
state of balance - There must be no unbalanced
or equality moments acting on the body.
between
opposing
forces." What
two
requirements
must be met in
order to be
considered in a
state of
equilibrium?
, An airplane is 33.4 degrees
climbing at a
constant
airspeed in no-
wind conditions.
The plane is
directly over a
point on the
ground that is 3
nautical miles
from the takeoff
point and the
altimeter reads
12,000 feet. Find
the plane's climb
angle in degrees.
Updated Questions and Correct
Answers | Graded A+ | Verified
Answers | Just Released (Latest
Version)
Save
Terms in this set (131)
Aerodynamic Lift and Drag
Force (AF)
resolves into
which two
aerodynamic
components?
,The aerodynamic Lift
component that
is 90 ° to the
flight path and
acts toward the
top of the
airplane is
called:
The aerodynamic Drag
component that
is parallel to the
flight path and
acts toward the
rear of the
airplane is
called:
The measure of Mass
the amount of
material
contained in a
body is called:
,The force Weight
influenced by
the gravitational
attraction of the
earth, moon, or
sun is called:
Equilibrium is - There must be no unbalanced
defined as "a forces acting on the body.
state of balance - There must be no unbalanced
or equality moments acting on the body.
between
opposing
forces." What
two
requirements
must be met in
order to be
considered in a
state of
equilibrium?
, An airplane is 33.4 degrees
climbing at a
constant
airspeed in no-
wind conditions.
The plane is
directly over a
point on the
ground that is 3
nautical miles
from the takeoff
point and the
altimeter reads
12,000 feet. Find
the plane's climb
angle in degrees.
