Automated optimum design of wing structures: A probabilistic approach

Author:

Rao S.S.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modeling and Simulation,Civil and Structural Engineering

Reference16 articles.

1. A theoretical analysis of undercarriage loads and taxi vibration on a supersonic transport aircraft;Mitchell;RAE TR 70173,1970

2. Analytical and experimental studies on dynamic loads in airplane structures during landing;Pian;J. Aeronaut. Sci.,1950

3. Analytical and experimental studies on dynamic loads in airplane structures during landing;Pian;J. Aeronaut. Sci.,1950

4. Effect of interaction on landing-gear behavior and dynamic loads in a flexible airplane structure;Cook;NACA Report 1278,1956

5. The analysis of dynamic stresses in aircraft structures during landing as nonstationary random processes;Fung;J. appl. Mech.,1955

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1. Fully Parametric Optimization Designs of Wing Components;International Journal of Aerospace Engineering;2020-10-14

2. Stochastic Programming;Engineering Optimization Theory and Practice;2019-10-22

3. Interval-Based Multiobjective Optimization of Aircraft Wings Under Gust Loads;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07

4. Interval-Based Multi-Objective Optimization of Aircraft Wings Under Gust Loads;AIAA Journal;2009-03

5. Interval-based optimization of aircraft wings under landing loads;Computers & Structures;2009-02

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