INTEGRAL SOLUTION OF UNSTEADY FULL-POTENTIAL EQUATION FOR A TRANSONIC PITCHING AIRFOIL

被引:5
|
作者
KANDIL, OA
HU, H
机构
[1] Old Dominion University, Norfolk, VA
[2] Department of Mechanical Engineering and Mechanics, Hampton University
来源
JOURNAL OF AIRCRAFT | 1990年 / 27卷 / 02期
关键词
D O I
10.2514/3.45907
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The unsteady full-potential equation formulation in a moving frame of reference has been developed and used to solve unsteady transonic flow problems. An unsteady integral-equation shock-capturing (IE-SC) scheme has been developed. The resulting unsteady IE-SC scheme is applied to a NACA 0012 airfoil undergoing a pitching oscillation. The numerical results are compared with those of an implicit, approximately factored, finite-volume Euler scheme. The present scheme is efficient in terms of the number of iterations as compared to the other existing schemes, which use finite-difference or finite-volume methods. © 1989 American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
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页码:123 / 130
页数:8
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