A hybrid inverse optimization method for the aerodynamic design of lifting surfaces-Reference-Cited by-同舟云学术

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A hybrid inverse optimization method for the aerodynamic design of lifting surfaces

Published:1994-06-20 Issue: Volume: Page:
ISSN:
Container-title:12th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Santos Luis¹

Affiliation:

1. Embraer - Empresa Brasileira de Aeronautica, S.A., Sao Jose dos Campos, Brazil

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1895

Reference24 articles.

1. AGARD-CP-463, "Computational Methods for Aerodynamic Design (Inverse)and Optimization," Neullysur-Seine,France,1990.

2. Thibert,J.J."One-point and Multi-point Design Optimization for Airplane and Helicopter Application" in AGARD-R-780 ( Inverse Design Methods for Airfoil Design for Aeronautical and Turbomachinery Applications),1989.

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1. Inverse Design of Airfoils Using Target Pressure Optimization;Advanced Materials Research;2013-05

2. Characteristics-based Boundary Conditions for the Euler Adjoint Problem: 2-D Formulation;28th AIAA Applied Aerodynamics Conference;2010-06-28

3. Engine-Airframe Integration Methodology for Regional Jet Aircrafts with Underwing Engines;41st Aerospace Sciences Meeting and Exhibit;2003-01-06

4. Application of Inverse Design Method to Estimation of Wind Tunnel Models;Inverse Problems in Engineering Mechanics IV;2003

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