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Publication:3741225
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zbMATH Open0604.73092MaRDI QIDQ3741225

A. Nastase

Publication date: 1985



Title of this publication is not available (Why is that?)


zbMATH Keywords

designinduced dragminimum draggeometrical characteristicscruising Mach numberfully-optimized integrated wingfuselage is located inside the thicknessgraphic-analytical methodincreased liftoptimum-optimorum integrated delta wingsimultaneously optimized


Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) General aerodynamics and subsonic flows (76G25) Optimization problems in solid mechanics (74P99) Supersonic flows (76J20)



Related Items (2)

Redesign of a supercritical wing in the presence of an engine nacelle ⋮ Title not available (Why is that?)






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