Airfoil Design by an All-at-once Method*
DOI10.1080/10618569808940863zbMath0940.76084OpenAlexW2121866348WikidataQ58048122 ScholiaQ58048122MaRDI QIDQ4248826
Matthias Heinkenschloss, A. R. Shenoy, Eugene M. Cliff
Publication date: 19 July 2000
Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/10618569808940863
nonlinear programmingconstrained optimization problemall-at-once approachoptimum airfoil design problemsteady state Euler equation
General aerodynamics and subsonic flows (76G25) Variational methods applied to problems in fluid mechanics (76M30) Flow control and optimization for compressible fluids and gas dynamics (76N25)
Related Items (18)
Uses Software
Cites Work
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- A comparison of optimization-based approaches for a model computational aerodynamics design problem
- An optimal control problem for flows with discontinuities
- Optimal control of two-and three-dimensional incompressible Navier-Stokes flows
- A PDE sensitivity equation method for optimal aerodynamic design
- Surface boundary conditions for the numerical solution of the Euler equations
- Problem Formulation for Multidisciplinary Optimization
- Projected Sequential Quadratic Programming Methods
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