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Previous year question hub

Numerical Methods - Engineering Mathematics - Aerospace Engineering Previous Year Questions

Practice Numerical Methods - Engineering Mathematics - Aerospace Engineering previous year questions organised from real papers, with year-wise coverage and clear topic navigation.

2Papers
2Years
2Questions
1Topics

Numerical Methods question pattern

Every graph below is calculated only from this selection.

Questions by year

Year-wise coverage for Numerical Methods. Each bar uses a separate theme-derived color.

Difficulty distribution

How the classified questions are distributed by difficulty.

Easy 1 50%
Medium 1 50%

Question type distribution

MCQ, numerical, multiple-select and other formats found in these papers.

Numerical Answer Type (NAT) 2 100%

Subject weightage

Top subjects by unique question coverage.

Aerospace Engineering
2 Qs

Most asked topics

Top topics across the included previous year papers.

Engineering Mathematics
2 Qs

Subtopic coverage

Top subtopics inside this exact selection.

Numerical Methods
2 Qs

Paper coverage

Question coverage for the most populated papers. Every active PYP paper remains listed below.

Aerospace Engineering (AE) 2026
1 Qs
Aerospace Engineering (AE) 2025
1 Qs

Included previous year papers

Newest papers appear first. Sort by year, question coverage or name.

PaperYear / sessionQuestions in this viewOpen
Aerospace Engineering (AE) 202620261View paper
Aerospace Engineering (AE) 202520251View paper

All Numerical Methods previous year questions

Practice every matching question in batches of 20, with every available option.

1
2025 · Aerospace Engineering · Engineering Mathematics · Numerical Methods
Aerospace Engineering (AE) 2025
An approximate solution of the equation \(x^3 - 17 = 0\) is to be obtained using the Newton-Raphson method. If the initial guess is \(x_0 = 2\), the value at the end of the first iteration is \(x_1 = \) ____ (rounded off to two decimal places).
Enter a numerical response
Open complete paper
2
2026 · Aerospace Engineering · Engineering Mathematics · Numerical Methods
Aerospace Engineering (AE) 2026
A furnace of 250 MW rating is used to melt and raise the temperature of aluminium from 25 °C to 900 °C. Aluminium has a solid-state specific heat, latent heat, and liquid-state specific heat of 0.9 kJ/kg·K, 390 kJ/kg, and 1.108 kJ/kg·K, respectively, and the furnace has 70% efficiency. The melting point of aluminium is 660 °C. The amount of aluminium that can be processed per hour is __________ kg (rounded off to 1 decimal place).
Enter a numerical response
Open complete paper