GATE 2026 AE Question Paper with Solutions (Available)- Download Pdf

The question paper and solution PDF of the Aerospace Engineering paper is available here. The exam ‌for GATE 2026 AE paper was scheduled for 7th February, session 1 (2:30 PM to 5:30 PM).

The GATE 2026 AE exam happens for 100 marks, where 15 marks come from the general aptitude section, 13 marks from Engineering mathematics. The remaining 72 marks come from core subjects.

Based on the initial analysis, the AE question paper was considered moderate to tough. To rank under 1000 in Instrumentation, you need to score 55-60+ marks out of 100.

GATE 2026 AE Question Paper with Solution PDF (Memory- Based)

GATE 2026 Aerospace Engineering (AE) Question Paper with Solution PDF	Download	Check Solutions

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Question 1:

For a subsonic flow over an airfoil, an increase in velocity leads to:

(A) Increase in pressure
(B) Decrease in pressure
(C) No change in pressure
(D) Zero pressure
(E) None of the above

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Question 2:

Which of the following motions is primarily associated with lateral stability of an aircraft?

(A) Pitch
(B) Roll
(C) Yaw
(D) Heave
(E) Surge

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Question 3:

Which propulsion system is most suitable for high-speed supersonic aircraft?

(A) Turboprop
(B) Turbojet
(C) Turbofan
(D) Ramjet
(E) Piston Engine

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Question 4:

The primary load-carrying structural component of an aircraft wing is:

(A) Rib
(B) Stringer
(C) Spar
(D) Skin
(E) Bulkhead

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Question 5:

For an isentropic flow of a perfect gas, an increase in Mach number results in:

(A) Increase in temperature
(B) Decrease in temperature
(C) Constant temperature
(D) Infinite temperature
(E) Zero temperature

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Question 6:

Which control surface is mainly used to control the yaw motion of an aircraft?

(A) Aileron
(B) Elevator
(C) Rudder
(D) Flap
(E) Trim Tab

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Question 7:

The velocity required for a satellite to remain in a circular orbit close to Earth is called:

(A) Escape velocity
(B) Orbital velocity
(C) Terminal velocity
(D) Relative velocity
(E) Critical velocity

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GATE 2026 Question Paper

GATE Questions

1.
A plate of 30 mm thickness is fed through a rolling mill with two powered rolls. Each roll has a diameter of 500 mm. The plate thickness is to be reduced to 27 mm in a single pass. Assume no change in width. The process feasibility and the maximum draft (in mm) can be represented, respectively, as
Use the coefficient of friction as 0.12

NOT feasible and 6.0
NOT feasible and 2.6
feasible and 3.6
feasible and 3.0

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2.
The values of a function \( f \) obtained for different values of \( x \) are shown in the table below.
Using Simpson’s one-third rule, approximate the integral \[ \int_0^1 f(x) \, dx \quad \text{(rounded off to 2 decimal places)}. \]

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3.
The welding process commonly used for fabricating tailor-welded blanks of dissimilar thickness for automotive applications is

arc welding
laser welding
gas welding
friction welding

View Solution

4.
The state of stress at a point is shown in the figure given below. Under plane stress assumption, the normal strain along the thickness direction (\(\epsilon_{zz}\)) is _________ (rounded off to 2 decimal places).

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5.
A truss structure is loaded as shown in the figure below. Among the options given, which member in the truss is a zero-force member?
\[ {Given: } F = 1000\,{N} \]

\(BD\)
\(BC\)
\(BA\)
\(AD\)

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6.
A vibrating system has a critical damping coefficient \(C_c = 350 \, \text{N}\cdot\text{s/m}\) and an actual damping coefficient \(C = 35 \, \text{N}\cdot\text{s/m}\). The logarithmic decrement of the system is approximately:

0.10
0.31
0.63
3.14

View Solution

GATE 2026 AE Question Paper with Solutions (Available)- Download Pdf

GATE 2026 AE Question Paper with Solution PDF (Memory- Based)

GATE 2026 Question Paper

GATE Questions

2.
The values of a function \( f \) obtained for different values of \( x \) are shown in the table below.
Using Simpson’s one-third rule, approximate the integral \[ \int_0^1 f(x) \, dx \quad \text{(rounded off to 2 decimal places)}. \]

3.
The welding process commonly used for fabricating tailor-welded blanks of dissimilar thickness for automotive applications is

4.
The state of stress at a point is shown in the figure given below. Under plane stress assumption, the normal strain along the thickness direction (\(\epsilon_{zz}\)) is _________ (rounded off to 2 decimal places).

5.
A truss structure is loaded as shown in the figure below. Among the options given, which member in the truss is a zero-force member?
\[ {Given: } F = 1000\,{N} \]

6.
A vibrating system has a critical damping coefficient \(C_c = 350 \, \text{N}\cdot\text{s/m}\) and an actual damping coefficient \(C = 35 \, \text{N}\cdot\text{s/m}\). The logarithmic decrement of the system is approximately:

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GATE 2026 AE Question Paper with Solution PDF (Memory- Based)

GATE 2026 Question Paper

GATE Questions

2.The values of a function \( f \) obtained for different values of \( x \) are shown in the table below.Using Simpson’s one-third rule, approximate the integral \[ \int_0^1 f(x) \, dx \quad \text{(rounded off to 2 decimal places)}. \]

3.The welding process commonly used for fabricating tailor-welded blanks of dissimilar thickness for automotive applications is

4.The state of stress at a point is shown in the figure given below. Under plane stress assumption, the normal strain along the thickness direction (\(\epsilon_{zz}\)) is _________ (rounded off to 2 decimal places).

5.A truss structure is loaded as shown in the figure below. Among the options given, which member in the truss is a zero-force member?\[ {Given: } F = 1000\,{N} \]

6.A vibrating system has a critical damping coefficient \(C_c = 350 \, \text{N}\cdot\text{s/m}\) and an actual damping coefficient \(C = 35 \, \text{N}\cdot\text{s/m}\). The logarithmic decrement of the system is approximately:

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2.
The values of a function \( f \) obtained for different values of \( x \) are shown in the table below.
Using Simpson’s one-third rule, approximate the integral \[ \int_0^1 f(x) \, dx \quad \text{(rounded off to 2 decimal places)}. \]

3.
The welding process commonly used for fabricating tailor-welded blanks of dissimilar thickness for automotive applications is

4.
The state of stress at a point is shown in the figure given below. Under plane stress assumption, the normal strain along the thickness direction (\(\epsilon_{zz}\)) is _________ (rounded off to 2 decimal places).

5.
A truss structure is loaded as shown in the figure below. Among the options given, which member in the truss is a zero-force member?
\[ {Given: } F = 1000\,{N} \]

6.
A vibrating system has a critical damping coefficient \(C_c = 350 \, \text{N}\cdot\text{s/m}\) and an actual damping coefficient \(C = 35 \, \text{N}\cdot\text{s/m}\). The logarithmic decrement of the system is approximately: