The application of inverse boundary layer methods to the three-dimensional viscous design problem-Reference-Cited by-同舟云学术

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The application of inverse boundary layer methods to the three-dimensional viscous design problem

Published:1986-01 Issue:1 Volume:2 Page:57-61
ISSN:0748-8025
Container-title:Communications in Applied Numerical Methods
language:en
Short-container-title:Commun. Appl. Numer. Methods

Author:

Lekoudis S. G.,Sankar N. L.,Malone J. B.

Publisher

Wiley

Subject

General Engineering

Reference16 articles.

1. and . ‘The NYU inverse swept wing code’, NASA CR-3662 (1983).

2. and . ‘Computational aerodynamic design of advanced transport aircraft’, A.I.A.A. Paper 83-1865.

3. A Subsonic Panel Method for Iterative Design of Complex Aircraft Configurations

4. and . ‘A direct-inverse three-dimensional transonic wing design method for vector computers’, A.I.A.A. Paper 84-2150.

5. , and . ‘Turbulent drag characteristics of small amplitude rigid surface waves’, A.I.A.A. Paper 83-0228.

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. Aerodynamic shape design and optimization - Status and trends;Journal of Aircraft;1992-11

2. Inverse mode calculations of the incompressible turbulent boundary layer on an ellipsoid;AIAA Journal;1986-10

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