Difficulty distribution
How the classified questions are distributed by difficulty.
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Practice Heat Transfer - Fluid Mechanics and Thermal Sciences - Mechanical Engineering previous year questions organised from real papers, with year-wise coverage and clear topic navigation.
Every graph below is calculated only from this selection.
Year-wise coverage for Heat Transfer. Each bar uses a separate theme-derived color.
How the classified questions are distributed by difficulty.
MCQ, numerical, multiple-select and other formats found in these papers.
Top subjects by unique question coverage.
Top topics across the included previous year papers.
Top subtopics inside this exact selection.
Question coverage for the most populated papers. Every active PYP paper remains listed below.
Newest papers appear first. Sort by year, question coverage or name.
| Paper | Year / session | Questions in this view | Open |
|---|---|---|---|
| Mechanical Engineering (ME) 2026 | 2026 | 5 | View paper |
| Mechanical Engineering (ME) 2025 | 2025 | 3 | View paper |
| Mechanical Engineering (ME) 2024 | 2024 | 6 | View paper |
| Mechanical Engineering (ME) 2023 | 2023 | 5 | View paper |
| Mechanical Engineering (ME) 2021 [Session 1] | 2021 | 4 | View paper |
| Mechanical Engineering (ME) 2020 [Session 1] | 2020 | 2 | View paper |
| Mechanical Engineering (ME) 2020 [Session 2] | 2020 | 3 | View paper |
| Mechanical Engineering (ME) 2019 [Session 1] | 2019 | 4 | View paper |
| Mechanical Engineering (ME) 2019 [Session 2] | 2019 | 5 | View paper |
| Mechanical Engineering (ME) 2018 [Session 1] | 2018 | 1 | View paper |
| Mechanical Engineering (ME) 2018 [Session 2] | 2018 | 3 | View paper |
| Mechanical Engineering (ME) 2016 [Session 1] | 2016 | 4 | View paper |
| Mechanical Engineering (ME) 2016 [Session 2] | 2016 | 2 | View paper |
| Mechanical Engineering (ME) 2016 [Session 3] | 2016 | 4 | View paper |
| Mechanical Engineering (ME) 2014 [Session 1] | 2014 | 4 | View paper |
| Mechanical Engineering (ME) 2014 [Session 2] | 2014 | 5 | View paper |
| Mechanical Engineering (ME) 2014 [Session 3] | 2014 | 5 | View paper |
| Mechanical Engineering (ME) 2014 [Session 4] | 2014 | 5 | View paper |
| Mechanical Engineering (ME) 2013 [Session 1] | 2013 | 6 | View paper |
| Mechanical Engineering (ME) 2013 [Session 2] | 2013 | 6 | View paper |
| Mechanical Engineering (ME) 2013 [Session 3] | 2013 | 6 | View paper |
| Mechanical Engineering (ME) 2013 [Session 4] | 2013 | 6 | View paper |
| Mechanical Engineering (ME) 2011 | 2011 | 4 | View paper |
| Mechanical Engineering (ME) 2010 | 2010 | 1 | View paper |
| Mechanical Engineering (ME) 2009 | 2009 | 5 | View paper |
| Mechanical Engineering (ME) 2008 | 2008 | 5 | View paper |
| Mechanical Engineering (ME) 2007 | 2007 | 6 | View paper |
Practice every matching question in batches of 20, with every available option.
For flow of fluid over a heated plate, the following fluid properties are known: viscosity = 0.001 Pa.s; specific heat at constant pressure = 1 kJ/kg.K; thermal conductivity = 1 W/m.K. The hydrodynamic boundary layer thickness at a specified location on the plate is 1 mm. The thermal boundary layer thickness at the same location is
The logarithmic mean temperature difference (LMTD) of a counterflow heat exchanger is 20°C. The cold fluid enters at 20°C and the hot fluid enters at 100°C. Mass flow rate of the cold fluid is twice that of the hot fluid. Specific heat at constant pressure of the hot fluid is twice that of the cold fluid. The exit temperature of the cold fluid

A hollow enclosure is formed between two infinitely long concentric cylinders of radii 1 m and 2 m, respectively. Radiative heat exchange takes place between the inner surface of the larger cylinder (surface-2) and the outer surface of the smaller cylinder (surface-1). The radiating surfaces are diffuse and the medium in the enclosure is non-participating. The fraction of the thermal radiation leaving the larger surface and striking itself is

Steady two-dimensional heat conduction takes place in the body shown in the figure below. The normal temperature gradients over surfaces P and Q can be considered to be uniform. The temperature gradient ∂T/∂x at surface Q is equal to 10 K/m. Surfaces P and Q are maintained at constant temperatures as shown in the figure, while the remaining part of the boundary is insulated. The body has a constant thermal conductivity of 0.1 W/m.K. The values of ∂T/∂x and ∂T/∂y at surface P are

In a condenser of a power plant, the steam condenses at a temperature of 60 °C. The cooling water enters at 30 °C and leaves at 45 °C. The logarithmic mean temperature difference (LMTD) of the condenser is
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