This chapter represents the studies (theoretical, numerical, and experimental) of geometric parameters’ effect on aerodynamic characteristics. Particularly, subchapters consider high-wing and low-wing, wingspan ratio, airfoils and angles of their setting, stagger and vertical gap between the wings, and wings’ dihedral angles. There is research on wingtip devices installed on forward and rear wings that affect not only lift-drag ratio but all three degrees of static stability as well. The chapter ends with a CFD study of aerodynamic features of folding design (tube-launched UAV that goes through different sweep angles of the wings immediately after its release).


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    Effect of Geometric Parameters on the Aerodynamic Characteristics of Grid-Fin Cells at Supersonic Speeds AIAA Paper

    Theerthamalai, P. / Balakrishnan, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007


    Effect of Geometric Scaling on Aerodynamic Performance

    Ronan Grimes / Ed Walsh / David Quin et al. | AIAA | 2005


    STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER

    Wang, B. / Yang, X. D. / Song, B. F. et al. | British Library Conference Proceedings | 2021


    Geometric, aerodynamic, and kinematic characteristics of two keel parawings during deployment

    Kenner, Paul M. / Churchill, Frederic T. / Holt, Ralph B. | TIBKAT | 1971