32th Congress of the International Council of the Aeronautical Sciences

03.1 - Aerodynamics – CFD Methods and Validation

FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE

H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia; M.A. Andira¹, R. Julistina¹, M.A. Moeljadi, Institute of Technology Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia

Based on results reported earlier, further CFD simulation-parametric study guided by a hypothetic flow situation depicting flow structure in and around the Coand? device is conducted. New CFD Simulation Studies are conducted for jet flow around half sphere at various relevant dimensions on the half sphere that may generate lift-thrust.


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