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WorksheetsAero Quiz
Total questions: 105
Worksheet time: 2hrs 45mins
What is aerodynamic ?
Car speed
The way air moves around things
The car body
Which shape is a good aerodynamic
1
2
3
Which car is the fastest ?
Which vehicle has low speed ?
Which car has a high speed ?
What is "Motion" ?
Is the process of something moving
Is opposite of moving
Is the friction
This picture is ...
Action
Friction
Motion
Reaction
Which of the pictures shows Motion ( Two Answers ?
This Pictures Shows ...
Friction
Newton
Aerodynamic
Friction is the opposite of motion .
False
True
Ideal fluid has
Static condition
Zero viscosity
constant viscosity
incompressible nature
Calculation of water pressure force on dam is the problem of
Statics
Kinetics
Kinematics
Dynamics
Fluid kinematics means study of
flow through venturimeter
pressure acting on closed sluice gate
Reynolds experiment
Determination of MG
Pitot tube measures
atmispheric pressure
Pressure in a car tyre
velocity of flow
piezometric pressure
Coefficient of discharge of a venturimeter is
1.1
9.81
0.9
.5
For laminar flow in a pipe Reynold's number should be
less than 500
more than 4000
less than 2000
1
Locus of all points emerging from single reference point known as
streamline
path line
equipotential line
streak line
Friction factor depends on
Reynolds number
diameter of pipe
roughness of pipe material
all of above
The unit of kinematic viscosity is
Pa.s
Sq.m per sec
Pa.sec / sq. m
Kg.sec sq. / sq. m
The constant discharge passing through an uniform dia. pipe is
Unsteady uniform
nonuniform unsteady
uniform steady
Laminar flow
Poise is the unit of
Mass density
Kinematic viscosity
viscosity
velocity gradient
A Newtonion fluid is defined as the fluid which
is incompatible and non-viscous
Obeys Newton's law of viscosity
is higly viscous
is compressible and viscous
Which of the following represent the major energy loss
Bend in pipe
Pipe fittings
Sudden exoansion
Friction loss
The following are the three different types of test signals used to test the response of a control system, except:
Step signal
Transient signal
Ramp signal
Parabolic signal
How would be the response of a stable control system be when it's given a bounded input signal?
Unbounded output
Bounded output
None of the above
Upon solving for the roots of a characteristic equation, you find that:
i. 2 roots are in the left half of the s-plane
ii. 2 simple roots are lying on the jw (imaginary axis), and
iii. 1 root is in the right half of the s-plane
What can you conclude about the system stability?
The system is marginally stable
The system is stable
The system is unstable
What method can you use to determine the stability of a control system without solving for the roots of the characteristic equation?
Routh-Hurwitz Criterion
Polynomial root calculation
Auxiliary equation formation method
While using the Routh-Hurwitz (RH) criterion for the characteristic equation of a CLTF, you find that there a 2 sign changes in the 1st column of the RH table. What is the most likely cause of this? What's your conclusion?
2 simple roots on the imaginary axis; system is marginally stable
2 roots of the left half of the s-plane; system is stable
2 roots on the right half of the s-plane; system is unstable
2 roots on the right half of the s-plane; system is stable
Δ(s) =s2+7s+20
The above is the characteristic equation of a system. Calculate the values of the damping ratio and natural undamped frequency, respectively.
0.783 and 4.472, respectively
4.472 and 0.783, respectively
0.175 and 20, respectively
20 and 0.175, respectively
How do you determine the damping type for a particular system?
By finding the value of it's natural undamped frequency
By finding the value of its damping factor
By finding the value of its damping ratio
By looking at its step response graph
G(s)=(s+5)(s+4)100
Calculate the steady-state error for a system with the above open-loop transfer function. Given the input is a unit step signal.
5
Zero error
Infinite error
0.1667
Design, building, analysis, and troubleshooting of components in aircraft, spacecraft, missiles, and high-altitude vehicles.
Aeronautics
Propulsion System
Elevator
Aerospace Engineering
Aerodynamic force created by the friction of moving air that opposes propulsion.
Angle of Attack
Drag
Thrust
Aileron
Theory that states an airfoil is more curved on the top, so air traveling over the wing has to travel farther than the air traveling under the wing, causing the air flowing over the wing to flow faster relative to the wing than the air flowing under the wing, causing a low pressure zone above the wing and, therefore, lift.
Bernoulli theory of lift
Pitch
Aerospace engineering
Diherdral Angle
Study of manned and unmanned craft outside the earth’s atmosphere
Gas turbine engine
Rudder
Astronautics
Aileron
Control surface located on the rear of the horizontal stabilizer that controls vertical movement of the nose.
Gas turbine engine
Astronautics
Propulsion system
Elevator
Rotating blades that force air toward the rear of an aircraft causing the aircraft to move forward.
Satellite
Elevator
Aerospace Engineering
Propeller
Angle of the chord line of the wing relative to the airflow.
Aerospace Engineering
Satellite
Angle of attack
Wind turbine
Upward angle of wings away from the body that creates stability.
Aeronautics
Dihedral angle
Satellite
Astronautics
Component of a wing that is located on the outside rear of each wing and is adjusted for turning.
Gas turbine engine
Aileron
Propeller
Flap
Type of spacecraft that orbits the earth because the centrifugal force created by its motion is in perfect balance with the earth’s gravitational pull.
Aileron
Propeller
Flap
Satellite
Airplane component that is located on the inside rear of wings and can be adjusted at takeoff and landing for additional lift.
Aeronautics
Dihedral angle
Flap
Aileron
Angle of the wing in relation to the airplane body.
Aileron
Satellite
Flap
Angle of incidence
Forward force acting on an aircraft or spacecraft created by air or gases being pushed to the rear.
Angle of incidence
Thrust
Drag
Aileron
System that creates thrust for movement.
Aeronautics
Propulsion System
Lift
Propeller
Engine, also known as a jet engine, that pulls air into the front of the engine, increases the pressure of the air, and forces it out the back of the engine at great speed.
Rudder
Gas turbine engine
Aerospace engineering
Angle of attack
Control surface located on the rear of the vertical stabilizer, used to control side-to-side movement of the nose.
Rudder
Gas turbine engine
Lift
Propulsion
Type of windmill used to generate electricity from wind energy.
Wind turbine
Yaw
Aerodynamics
Pitch
Which of the following are not created by a physical contact between an aircraft and the air around it?
Drag
Gravity
Lift
All of the above
_____ defined laws of motion that have had a tremendous impact on aerospace engineering.
Blaise Pascal
Neils Bohr
Robert Boyle
Sir Isaac Newton
The more aerodynamic a plane is, the more efficiently it will fly.
True
False
The earth orbits satellites in much the same way the earth orbits the sun.
True
False
_____ is the study of how air flows around solid objects.
Aeronautics
Aesthetics
Aerodynamics
Ailerons
Rocket engines can operate in space because there is a limitless amount of oxygen.
True
False
All of the electronic devices and systems which perform individualized functions, used on any aircraft are called …
Flight Control System
Avionics System
Aviation System
Navigation System
What is the component in the HF Radio Communication used for transmitting and receiving the signal?
HF antenna
VHF antenna
HF transceiver
HF coupler
What is ADF for?
It indicates station location when the aircraft is flying toward
It gives information about the distance to the DME Station that is going toward
It is for receiving and transmitting the signal.
It helps the pilot in seeing the runway
What is DME for?
It indicates station location when the aircraft is flying toward
It gives information about the distance to the DME Station that is going toward
It is for receiving and transmitting the signal.
It helps the pilot in seeing the runway
Which one of the followings is NOT function of the aircraft’s avionic equipment in the cockpit?
For communication
For Navigation
For monitoring
For decorating
Where is the location of HF antenna?
Top of fuselage
Bottom of fuselage
Horizontal Stabilizer
Vertical Stabilizer
What does ADF stand for?
Automatic Direction Finder
Automatic Direction Finger
Automatic Duration Finder
Aircraft Direction Finder
What does DME stand for?
Direction Measuring Equipment
Distance Monitoring Equipment
Duration Measuring Equipment
Distance Measuring Equipment
What is the majority of aircraft power used in avionics?
14-28 VDC and 115 Hz 400 VAC
14-28 VDC and 400 Hz 150 VAC
14-28 VDC and 400 Hz 115 VAC
4-28 VDC and 400 Hz 115 VAC
Which one is NOT the component of ADF?
ADF receiver
trim tab
antenna
bearing indicator
(Time: 20s) Guess the word which fits all 4 images.(6 letters)
_ _ _ _ _ _
(a)
(Time: 20s) Guess the word which fits all 4 images.(9 letters)
D _ _ _ _ _ _ _ Y
(a)
(Time: 20s) Guess the word which fits all 4 images.(8 letters)
_ _ _R L _ _ _
(a)
(Time: 20s) Guess the word which fits all 4 images.(5 letters)
F _ _ _ _
(a)
(Time: 20s) Guess the word which fits all 4 images.(9 letters)
_ _ _ _ _ T _ _ _
(a)
(Time: 20s) Guess the word which fits all 4 images.(4 letters)
_ _ _ _
(a)
(Time: 30s) Spot all the differences between the 2 images.
Mention the number of differences in the answer.
Eg.: 3 or three
(a)
(Time: 20s) Spot all the differences between the 2 images.
Mention the number of differences in the answer.
Eg.: 3 or three
(a)
(Time: 20s) Solve this.
(a)
(Time: 10s) Pick the odd one out
A
B
C
D
(Time: 20s) Guess the Disney movie name(3 words)
_ _ _ / _ _ _ _ _ _ / _ _ _ _
(a)
(Time: 10s) Guess the ice cream parlor name (2 words)
(a)
(Time: 10s) Guess the Disney movie name.(1 word)
(a)
(Time: 10s) Guess the hidden word
(a)
(Time: 5s) Which is correct logo A or B ?
(a)
