2021
DOI: 10.2514/1.d0190
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Multidisciplinary and Multi-Objective Optimization Considering Aircraft Program Cost and Airline Network

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Cited by 4 publications
(8 citation statements)
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“…[A] • {S} ≤ 0 (116) [B] • {S} = 0 (117) where [A] contains the gradients of inequality constraints only if they are active (with the safety margin term θ from Equation ( 109) dropped), and [B] contains the gradients of the equality constraints.…”
Section: Methods Of Feasible Directions and Modified Methods Of Feasi...mentioning
confidence: 99%
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“…[A] • {S} ≤ 0 (116) [B] • {S} = 0 (117) where [A] contains the gradients of inequality constraints only if they are active (with the safety margin term θ from Equation ( 109) dropped), and [B] contains the gradients of the equality constraints.…”
Section: Methods Of Feasible Directions and Modified Methods Of Feasi...mentioning
confidence: 99%
“…This may not be the case for regional airplanes, which perform the cruise phase is shorter when compared with long-haul airplanes. This type of airplane should be optimized for the airline network they will operate [17]. Table 2 shows the average stage length flown in the United States of some major airlines [18].…”
Section: The Quest For High Aspect-ratio Wings and New Aircraft Confi...mentioning
confidence: 99%
“…An in-house generic turbofan engine model is also part of the MDO framework [40]. It is possible to analyze the performance, emissions, and operational costs for missions inside a complex airline network with different takeoff weights or block distances [41]. The fuel storage capacity is precisely calculated considering the actual airplane geometry and structural layout.…”
Section: Introductionmentioning
confidence: 99%
“…A great deal of computational analysis is required to obtain optimum configurations to satisfy many objectives and design constraints. Disciplines such as aerodynamics, propulsion, flight mechanics, structures, and aeroelasticity, among others, are frequently considered in the optimization framework to obtain more realistic geometries of flight vehicles and, recently, the addition of flight profile and mission analysis has been added [28]. Nowadays, many design variables (and types) may be employed, and advanced optimization algorithms that enable complex models of the aeronautical disciplines may be considered.…”
Section: Introductionmentioning
confidence: 99%
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