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opprah-maker / Aircraft-Aerodynamics-Design

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Combined aerospace engineering project: NACA 0012 wind-tunnel aerodynamics (lift and drag polars, stall onset) plus heavy-lift transport aircraft conceptual sizing (W/S, T/W, Cn_beta).

matlab aerodynamics aerospace-engineering aircraft-design conceptual-design fluid-mechanics drag-coefficient experimental-methods lift-coefficient thrust-to-weight aircraft-sizing stability-derivatives wind-tunnel-testing naca-0012 directional-stability stall-analysis wing-loading vertical-tail
  • Updated Jun 6, 2026
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