A more accurate transonic computational method for wing-body configurations-Reference-Cited by-同舟云学术

A more accurate transonic computational method for wing-body configurations

Published:1983-06 Issue:6 Volume:21 Page:848-855
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chen L. T.¹

Affiliation:

1. McDonnell Douglas Corporation, St. Louis, Missouri

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.8162

Reference17 articles.

1. Progress in Finite-Volume Calculations for Wing-Fuselage Combinations

2. 3Chmielewski, G. E. 'Transonic Wing/Body Flow Analysis Using Non-Surface-Fitted Coordinates," AIAA Paper 81-0384, Jan. 1981.

3. 4Bailey, F. R. and Ballhaus, W. F. "Relaxation Methods for Transonic Flow About Wing-Cylinder Combinations and Lifting Swept Wings," Lecture Notes in Physics, Vol.19, Springer-Verlag, 1972, pp.3-9.

4. Computational transonic flow about realistic aircraft configurations

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