An inverse code based on a residual-correction method for wing design-Reference-Cited by-同舟云学术

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An inverse code based on a residual-correction method for wing design

Published:1999-06 Issue:4 Volume:3 Page:201-214
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Jiménez-Varona José

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Summary of design activities in LARA task 1.2;Bartelheimer;Technical Report LARA LTR-34,1995

2. The NYU inverse swept wing code;Bauer;Contractor Report,1983

3. Technique for developing design tools from the analysis methods of computational aerodynamics;Davis,1979

4. A criteria for surface pressure specification in aerodynamic shape design;Dulikravich,1990

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A new study for aeroplane wing shapes made of boron nitride nanotubes-reinforced aluminium, Part I: review, dynamical analyses and simulation;Composite Structures;2023-01

2. Two-Level Wing-Body-Fairing Optimization of a Civil Transport Aircraft;Journal of Aircraft;2011-11

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