MENG 628

Advanced Aerodynamics

New York Institute of Technology · UGRD · Fall 2026

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Review of basic incompressible and compressible flows, introduction to oblique shock waves, Prendtl-Meyer flows. Detailed airfoil analyses including effects on life and drag of angle of attack, Reynolds number, compressibility. Three-dimensional considerations: qualitative discussion of down-wash and circulation, quantitative aspects of this type of flow. Boundary layer theory: simple ideas, flat plate flows, calculation formulae.

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Class #new_york_2-MENG628Fall 2026UGRD3.0 credits
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