34th Aerospace Sciences Meeting and Exhibit 1996
DOI: 10.2514/6.1996-554
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Business jet wing design using aerodynamic shape optimization

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Cited by 14 publications
(10 citation statements)
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“…The first major industrial application of an adjoint based aerodynamic optimization method was the wing design of the Beech Premier [58] in 1995. The method was successfully used in inverse mode as a tool to obtain pressure distributions favorable to the maintenance of natural laminar flow over a range of cruise Mach numbers.…”
Section: Industrial Experience and Results Of Optimizationmentioning
confidence: 99%
See 1 more Smart Citation
“…The first major industrial application of an adjoint based aerodynamic optimization method was the wing design of the Beech Premier [58] in 1995. The method was successfully used in inverse mode as a tool to obtain pressure distributions favorable to the maintenance of natural laminar flow over a range of cruise Mach numbers.…”
Section: Industrial Experience and Results Of Optimizationmentioning
confidence: 99%
“…Consequently, the boundary contribution to the cost function M cannot be specified arbitrarily. Instead, it must be chosen from the class of functions which allow cancellation of all terms containing δw in the boundary integral of equation (58). On the other hand, there is no such restriction on the specification of the field contribution to the cost function P, since these terms may always be absorbed into the adjoint field equation (59) as source terms.…”
Section: Three-dimensional Design Using the Compressible Euler And Namentioning
confidence: 99%
“…The majority of work in aerodynamic shape optimisation has focused on the design of aerospace vehicles in a steady flow environment. Investigators have applied these advanced design algorithms, particularly the adjoint method, to numerous problems, ranging from the design of two-dimensional airfoils to full aircraft configurations to decrease drag, increase range and reduce sonic boom (Jameson 1989, Reuther et al 1992, Gallman et al 1996, Reuther et al 1999, Giles et al 2003, Leoviriyakit and Jameson 2004, Nemec et al 2004, Soto et al 2004, Mohammadi and Pironneau 2005, Mavriplis 2006). These problems have been tackled using many different numerical schemes on both structured and unstructured grids (Elliot and Peraire 1996, Anderson and Venkatakrishnan 1999, Nielsen et al 2004, Kim and Nakahashi 2005.…”
Section: Introductionmentioning
confidence: 99%
“…The majority of work in aerodynamic shape optimization has focused on the design of aerospace vehicles in a steady flow environment. Investigators have applied these advanced design algorithms, particularly the adjoint method, to numerous problems, ranging from the design of two-dimensional airfoils to full aircraft configurations to decrease drag, increase range, and reduce sonic boom (Jameson 1989;Reuther et al 1992;Gallman et al 1996;Reuther et al 1999;Kasidit and Jameson 2004;Mavriplis 2006;Soto et al 2004;Giles et al 2003;Nemec et al 2004;Mohammadi and Pironneau 2005). Researchers have tackled these problems using many different numerical schemes on both structured and unstructured grids (Kim and Nakahashi 2005;Nielsen et al 2004;Elliot and Peraire 1996;Anderson and Venkatakrishnan 1999).…”
mentioning
confidence: 99%