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Non-Linear Aeroelastic Predictions for Transport Aircraft The Boeing Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Purcell, T. W., author.
Conference Name:
Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
AbstractA loosely coupled method for aeroelastic predictions of aircraft configurations is shown. This method couples an advanced structural analysis method with a CFD aerodynamics code in a modular fashion. This method can use almost any CFD code, so a validation of several such codes is shown to establish regions of validity for each code. Results from potential codes, an Euler code, and a Navier-Stokes code are shown in comparison with experiment. Viscous effects are included in most cases through a coupled boundary-layer solver or a turbulence model as appropriate
Notes:
Vendor supplied data
Publisher Number:
901852
Access Restriction:
Restricted for use by site license

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