The hodograph, fictitious gas, inverse and numerical optimization approaches are discussed for transonic wing and airfoil design. It is suggested that if a general design method for complete wings is required neither the fictitious gas method nor the local residual-correction type of inverse approach are adequate. An inverse approach allowing global wing design as well as local design modifications is the best compromise, numerical optmization being too expensive.
Computational Procedures in Transonic Aerodynamic Design
1982
27 pages
Report
Keine Angabe
Englisch
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