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GATE Aerospace Engineering Exam (MCQ Only ) - English

Duration: 180 · Questions: 60 · Max Marks: 60 · Language: 1

View GATE Aerospace Engineering 2027 Exam Page

General Aptitude

1
Inhaling the smoke from a burning _____ could _____ you quickly.
  1. A.tire/tier
  2. B.tire/tyre
  3. C.tyre/tire
  4. D.tyre/tier
2
Rice, a versatile and inexpensive source of carbohydrate, is a critical component of diet worldwide. Climate change, causing extreme weather, poses a threat to sustained availability of rice. Scientists are working on developing Green Super Rice (GSR), which is resilient under extreme weather conditions yet gives higher yields sustainably.
Which one of the following is the CORRECT logical inference based on the information given in the above passage ?
  1. A.GSR is an alternative to regular rice, but it grows only in an extreme weather
  2. B.GSR be used in future in response to adverse effects of climate change
  3. C.GSR grows in an extreme weather, but the quantity of produce is lesser than regular rice
  4. D.Regular rice will continue to provide good yields even in extreme weather
3
The cost price of 20 articles is the same as the selling price of x articles. If the profit is 25%, then the value of x is :
  1. A.15
  2. B.16
  3. C.18
  4. D.25
4
Pipes P and Q can fill a storage tank full of water in 10 and 6 minutes, respectively. Pipe R draws the water out from the storage tank at a rate of 34 litres per minute. P, Q and R operate at a constant rate. If it takes one hour to completely empty a full storage tank with all the pipes operating simultaneously, what is the capacity of the storage tank (in litres) ? 
  1. A.26.8 
  2. B.60.0 
  3. C.120.0
  4. D.127.5
5
Choose the grammatically correct sentence?
  1. A.Neither of the robots are functioning properly
  2. B.Neither robots is functioning properly
  3. C.Neither of the robot are functioning properly
  4. D.Neither of the robots is functioning properly

Engineering Mathematics

1
Consider the following expression :
where z, y, and t are variables, and   is a complex number. The partial differential equation derived from the above expression is
    2
    For the equation
    the correct description is
    1. A.
      an ordinary differential equation of order 3 and degree 2 
    2. B.
      an ordinary differential equation of order 3 and degree 3 
    3. C.
      an ordinary differential equation of order 2 and degree 3 
    4. D.an ordinary differential equation of order 3 and degree â€‹
    3
    The value of (1 + i)12, where â€‹ , is.
    1. A.
      – 64 i 
    2. B.
      64 i
    3. C.64 
    4. D.– 64
    4
    If (A=\begin{bmatrix}1&2\3&4\end{bmatrix}), what is (\det(A))?
    1. A.2
    2. B.(-2)
    3. C.5
    4. D.10
    5
    If (A) is a (3\times3) matrix with (\det(A)=5), what is (\det(2A))?
    1. A.10
    2. B.40
    3. C.20
    4. D.80

    Aerospace Engineering

    1
    In the International Standard Atmosphere (ISA), the temperature lapse rate in the troposphere is:
    1. A.-6.5°C/km
    2. B.-5.5°C/km
    3. C.-7.5°C/km
    4. D.-4.5°C/km
    2
    The pressure at 10 km altitude in the ISA is approximately:
    1. A.36.5 kPa
    2. B.26.5 kPa
    3. C.46.5 kPa
    4. D.56.5 kPa
    3
    In the ISA, the density variation with altitude in the isothermal layer is:
    1. A.Constant
    2. B.Exponentially decreasing
    3. C.Linearly decreasing
    4. D.Linearly increasing
    4
    The primary structural component of an airplane wing responsible for lift is:
    1. A.Rib
    2. B.Skin
    3. C.Spar
    4. D.Stringer
    5
    A canard configuration refers to:
    1. A.A delta wing aircraft
    2. B.A tailless aircraft
    3. C.A wing with high aspect ratio
    4. D.A tail-first aircraft with a foreplane
    6
    In the ISA, the tropopause is located at an altitude of:
    1. A.11 km
    2. B.8 km
    3. C.15 km
    4. D.20 km
    7
    The primary function of the ailerons in an airplane is to control:
    1. A.Pitch
    2. B.Yaw
    3. C.Roll
    4. D.Thrust
    8
    The density of air at sea level in the ISA is:
    1. A.1.425 kg/m³
    2. B.1.325 kg/m³
    3. C.1.225 kg/m³
    4. D.1.525 kg/m³
    9
    A tailless aircraft configuration lacks:
    1. A.Vertical stabilizer
    2. B.Main wing
    3. C.Horizontal stabilizer
    4. D.Fuselage
    10
    The temperature at 15 km altitude in the ISA is approximately:
    1. A.-36.5°C
    2. B.-46.5°C
    3. C.-56.5°C
    4. D.-66.5°C
    11
    The primary purpose of the fuselage in an airplane is to:
    1. A.House the payload and systems
    2. B.Provide lift
    3. C.Control yaw
    4. D.Generate thrust
    12
    In the ISA, the speed of sound at sea level is approximately:
    1. A.320 m/s
    2. B.340 m/s
    3. C.360 m/s
    4. D.300 m/s
    13
    A monoplane differs from a biplane in having:
    1. A.One wing instead of two
    2. B.No tail
    3. C.A single engine
    4. D.A canard configuration
    14
    The pressure variation with altitude in the troposphere follows:
    1. A.Linear decrease
    2. B.Constant pressure
    3. C.Exponential decrease
    4. D.Quadratic decrease
    15
    The primary function of the vertical stabilizer is to:
    1. A.Control pitch
    2. B.Control roll
    3. C.Provide lift
    4. D.Control yaw
    16
    In the ISA, the temperature remains constant in the:
    1. A.Troposphere
    2. B.Stratosphere
    3. C.Mesosphere
    4. D.Thermosphere
    17
    The primary structural component that maintains the shape of the wing is:
    1. A.Spar
    2. B.Skin
    3. C.Stringer
    4. D.Rib
    18
    A delta wing configuration is characterized by:
    1. A.Triangular shape
    2. B.High aspect ratio
    3. C.Rectangular shape
    4. D.Swept-back shape
    19
    The primary function of flaps in an airplane is to:
    1. A.Reduce drag
    2. B.Control roll
    3. C.Control yaw
    4. D.Increase lift and drag
    20
    The altimeter measures altitude based on:
    1. A.Static pressure
    2. B.Dynamic pressure
    3. C.Total pressure
    4. D.Temperature
    21
    The indicated airspeed (IAS) is corrected for instrument and position errors to obtain:
    1. A.Equivalent airspeed (EAS)
    2. B.Calibrated airspeed (CAS)
    3. C.True airspeed (TAS)
    4. D.Mach number
    22
    The vertical speed indicator (VSI) measures:
    1. A.Rate of climb or descent
    2. B.Airspeed
    3. C.Altitude
    4. D.Heading
    23
    The Mach number is defined as:
    1. A.Ratio of calibrated airspeed to speed of sound
    2. B.Ratio of indicated airspeed to speed of sound
    3. C.Ratio of true airspeed to speed of sound
    4. D.Ratio of equivalent airspeed to speed of sound
    24
    The turn-bank indicator primarily shows:
    1. A.Pitch angle
    2. B.Altitude change
    3. C.Airspeed variation
    4. D.Rate of turn and coordination
    25
    Pressure altitude is defined as the altitude corresponding to:
    1. A.Dynamic pressure
    2. B.Local atmospheric pressure
    3. C.Standard pressure of 1013.25 hPa
    4. D.Total pressure
    26
    What is the standard sea-level temperature according to the International Standard Atmosphere?
    1. A.273.15 K
    2. B.303.15 K
    3. C.298.15 K
    4. D.288.15 K
    27
    What is the standard atmospheric pressure at mean sea level?
    1. A.101.325 kPa
    2. B.89.874 kPa
    3. C.110.250 kPa
    4. D.76.500 kPa
    28
    What is the standard sea-level density of air?
    1. A.0.925 kg/m³
    2. B.1.000 kg/m³
    3. C.1.500 kg/m³
    4. D.1.225 kg/m³
    29
    What is the approximate standard temperature lapse rate in the troposphere?
    1. A.3.25 K/km
    2. B.4.80 K/km
    3. C.9.81 K/km
    4. D.6.50 K/km
    30
    At approximately what altitude does the tropopause begin in the International Standard Atmosphere?
    1. A.5 km
    2. B.8 km
    3. C.11 km
    4. D.20 km
    31
    How does atmospheric pressure generally vary with increasing altitude?
    1. A.It increases linearly
    2. B.It first decreases and then becomes constant throughout the atmosphere
    3. C.It remains constant
    4. D.It decreases
    32
    Which equation relates atmospheric pressure, density and temperature for a perfect gas?
    1. A.Bernoulli equation
    2. B.Ideal gas equation
    3. C.Euler equation
    4. D.Momentum equation
    33
    Which two quantities primarily determine the hydrostatic pressure gradient in the atmosphere?
    1. A.Density and gravitational acceleration
    2. B.Velocity and viscosity
    3. C.Temperature and Mach number
    4. D.Dynamic pressure and altitude
    34
    On which atmospheric property does the local speed of sound in an ideal gas primarily depend?
    1. A.Static pressure only
    2. B.Static temperature
    3. C.Dynamic pressure only
    4. D.Relative humidity only
    35
    What is Mach number defined as?
    1. A.Ratio of true airspeed to local speed of sound
    2. B.Ratio of dynamic pressure to static pressure
    3. C.Ratio of equivalent airspeed to ground speed
    4. D.Ratio of calibrated airspeed to indicated airspeed
    36
    Which flight regime generally corresponds to an aircraft operating well below the local speed of sound?
    1. A.Subsonic
    2. B.Supersonic
    3. C.Hypersonic
    4. D.Hypervelocity
    37
    Which characteristic is most representative of transonic flow around an aircraft?
    1. A.The entire flow field is incompressible
    2. B.Local subsonic and supersonic regions coexist
    3. C.Shock waves cannot occur
    4. D.Local Mach number is zero everywhere
    38
    Which component of a conventional fixed-wing aircraft produces most of its aerodynamic lift?
    1. A.Vertical tail
    2. B.Main wing
    3. C.Fuselage
    4. D.Landing gear
    39
    What is the primary structural and functional role of an aircraft fuselage?
    1. A.To generate all aerodynamic lift
    2. B.To house crew, payload and major systems
    3. C.To provide roll control
    4. D.To eliminate induced drag
    40
    Which aircraft component primarily provides longitudinal stability and pitch control?
    1. A.Horizontal tail
    2. B.Vertical tail
    3. C.Wingtip
    4. D.Landing gear
    41
    Which aircraft component primarily contributes to directional static stability?
    1. A.Horizontal stabilizer
    2. B.Elevator
    3. C.Flap
    4. D.Vertical tail
    42
    Where is the horizontal tail located in a conventional airplane configuration?
    1. A.Ahead of the main wing
    2. B.Behind the main wing
    3. C.At the wing leading edge
    4. D.Beneath the landing gear
    43
    What distinguishes a canard configuration from a conventional tail configuration?
    1. A.A horizontal lifting/control surface is located ahead of the main wing
    2. B.The vertical tail is absent
    3. C.The main wing is always unswept
    4. D.The aircraft has no elevator-type control
    44
    Which primary flight-control surface controls aircraft pitch?
    1. A.Rudder
    2. B.Aileron
    3. C.Spoiler
    4. D.Elevator
    45
    Which primary flight-control surface is principally responsible for roll control?
    1. A.Aileron
    2. B.Elevator
    3. C.Rudder
    4. D.Flap
    46
    Which primary flight-control surface is principally responsible for yaw control?
    1. A.Elevator
    2. B.Rudder
    3. C.Aileron
    4. D.Slat
    47
    About which aircraft axis does rolling motion occur?
    1. A.Lateral axis
    2. B.Longitudinal axis
    3. C.Vertical axis
    4. D.Normal axis
    48
    About which aircraft axis does pitching motion occur?
    1. A.Lateral axis
    2. B.Longitudinal axis
    3. C.Vertical axis
    4. D.Flight-path axis
    49
    About which aircraft axis does yawing motion occur?
    1. A.Vertical axis
    2. B.Lateral axis
    3. C.Longitudinal axis
    4. D.Wing elastic axis
    50
    What does the angle of attack of a wing represent?
    1. A.Angle between wing chord and relative airflow
    2. B.Angle between wing span and horizon
    3. C.Angle between fuselage and runway
    4. D.Angle between vertical tail and fuselage