Subsonic and Transonic Flow Solutions Using Time Dependent Full Potential Equation

Author(s):  
Ahmet Ş. Üçer
1988 ◽  
Vol 92 (916) ◽  
pp. 235-241 ◽  
Author(s):  
P. M. Sinclair

Summary A three-dimensional integral formulation for the solution of the full potential equation and the associated numerical algorithm, the field-integral method, are presented. The method is a direct extension of a two-dimensional method and in particular retains the simple grid generation requirements noted in that method. Results are presented for the flow over body shapes and a complex winglet configuration, and are compared with existing transonic methods and experiments with good agreement. The further work necessary to provide a fast, robust method for use in design is outlined.


1985 ◽  
Vol 44 (169) ◽  
pp. 1-1 ◽  
Author(s):  
Stanley Osher ◽  
Mohamed Hafez ◽  
Woodrow Whitlow

1995 ◽  
Vol 48 (11S) ◽  
pp. S150-S157
Author(s):  
Mauri´cio Pazini Branda˜o

This paper reviews recent trends of analysis of aeroacoustic problems via traditional CFD techniques, as well as analysis of aerodynamic problems via modern aeroacoustic methods. Individual methods are described and tendencies of evolution are indicated. A generalized version of the full potential equation is derived. These two complementary forms of research converge towards the integration of Aeroacoustics and Aerodynamics into a single framework, where the computer serves as an integration tool.


AIAA Journal ◽  
1979 ◽  
Vol 17 (8) ◽  
pp. 838-844 ◽  
Author(s):  
M. Hafez ◽  
J. South ◽  
E. Murman

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