Official IIT Statistics & Cutoffs • 14-Year Subject Weightage Analysis • Recommended Reference Books • 3-Phase Roadmap • Target Score Planner
22 – 26 Marks (~24%)
Incompressible flow, thin airfoil theory, finite wing vortex systems, oblique shock waves, Prandtl-Meyer expansion, Rayleigh & Fanno flows.
20 – 24 Marks (~22%)
Gas turbine cycle analysis, turbojets & turbofans, subsonic/supersonic inlets, centrifugal & axial compressors, rocket thrust equation, nozzle expansion.
18 – 22 Marks (~20%)
Airplane performance in steady level flight, climb, glide & turn, static longitudinal & directional stability, dynamic modes (Phugoid, short period, Dutch roll).
16 – 20 Marks (~18%)
Bending, shear flow in open & closed thin-walled sections, shear center, torsion of thin-walled tubes, buckling of thin plates, structural dynamics.
Practice 1,105 official PYQs, attempt 50 full-length CBT mocks with virtual calculator, and download the 8-section formula sheet.