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The physical problem addressed was to find the aerodynamic forces acting on an V, U m/s Free stream air velocity. ρ kg/m3 Air density p N/m3 Static pressure. q N/m3 In the book Aerodynamics for Engineers [Bertin & Smith, 1998] the authors have provided a computational example of the VLM (p 291). Download pdf.

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Solution Manual for Aerodynamics for Engineers 6E John J. Bertin, Russell M. Cummings Instant download and all chapter Solution Manual for Aerodynamics for Engineers, 6E John J. Bertin, Russell M.Model tests of gliding with different hindwing configurations…https://pnas.org/contentBecause of the hindlimb posture, the biplane hindwings only provided 0.049 m2 of wing area, as opposed to >0.14 m2 for either of the abducted hindwings.

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