Transonic flow computations using nonlinear potential methods

被引:29
|
作者
Holst, TL [1 ]
机构
[1] NASA, Ames Res Ctr, Computat Phys & Simulat Branch, Moffett Field, CA 94035 USA
关键词
D O I
10.1016/S0376-0421(99)00010-X
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This presentation describes the state of transonic flow simulation using nonlinear potential methods for external-aerodynamic applications. The presentation begins with a review of the various potential equation forms (with emphasis on the full potential equation) and includes a discussion of pertinent mathematical characteristics and all derivation assumptions. Impact of the derivation assumptions on simulation accuracy, especially with respect to shock wave capture, is discussed. Key characteristics of all numerical algorithm types used for solving nonlinear potential equations, including steady, unsteady, space marching, and design methods, are described. Both spatial discretization and iteration scheme characteristics are examined. Numerical results for various aerodynamic applications are included throughout the presentation to highlight key discussion points. The presentation ends with concluding remarks and recommendations for future work. Overall, nonlinear potential solvers are efficient, highly developed and routinely used in the aerodynamic design environment for cruise conditions. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1 / 61
页数:61
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