Calculation of transonic flow by means of a shock-capturing field panel method-Reference-Cited by-同舟云学术

Calculation of transonic flow by means of a shock-capturing field panel method

Published:1979-07-23 Issue: Volume: Page:
ISSN:
Container-title:4th Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

PIERS W.¹,SLOOFF J.¹

Affiliation:

1. Nationaal Lucht- en Ruimtevaartlaboratorium, Amsterdam, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1459

Reference13 articles.

1. Brandt,A. Notebook AIAA Applied Aerod. Course, Albuquerque, June 1977. Rapid.finite-differencecomputation of subsonic and transonic aerodynamic flows 3 AIAA Paper No. 74-11. Accelarated Iterative Schemes for Transonic Flow Calculations Using Fast Poisson Solvers, "ERDA Report COO-3077-82, March 1975,New York University. Application of a multi-level grid method to transonic flow calculations, ICASE rep. 76-8 (1976).

2. TMX-73, 202,Jan. 1977NASA. L ?iehn. T,T ?nite difference methods for plane

3. Journ.Aircr. ,13.5 (137") 2:356. C&culat;ian of transonic wing flow by grid embedding ATAA Papr 77-ZUi"i' 1977. 22 Wartin, E. A fast semi-direct method for com

Cited by 16 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 fast higher-order integral equation method for solution of the full potential equation around airfoils;Engineering Analysis with Boundary Elements;2000-05

2. Field panel method with grid stretching technique for solving transonic potential flow around arbitrary airfoils;Computational Mechanics;1995-01

3. Development of a shock-fitting field-panel method for 3D transonic flows;Computational Mechanics;1995-01

4. Boundary integral equations and conservative dissipation schemes for full potential transonic flows;Computational Mechanics;1993-11

5. A 3D IEM for Compressible Wing Flows With and Without Shocks;Boundary Elements in Fluid Dynamics;1992