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panel method

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View Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment By Mark S. Chaffin

Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

By Mark S. Chaffin

View An approach to the design of airfoils with high lift to drag ratios By D. W. Zingg

An approach to the design of airfoils with high lift to drag ratios

An approach to the design of airfoils with high lift to drag ratios

By D. W. Zingg

View Development and analysis of panel methods for propellers in unsteady flow By Ching-Yeh Hsin

Development and analysis of panel methods for propellers in unsteady flow

Development and analysis of panel methods for propellers in unsteady flow

By Ching-Yeh Hsin

View CAR 88 By M. H. L. Hounjet

CAR 88

CAR 88

By M. H. L. Hounjet

View Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts By C. M. van Beek

Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts

Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts

By C. M. van Beek

View An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed By D. I. T. P. Llewelyn-Davies

An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed

An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed

By D. I. T. P. Llewelyn-Davies

View On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations By W. Loeve

On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations

On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations

By W. Loeve

View A new iterative matrix solution procedure for three-dimensional panel methods By R. W. Clark

A new iterative matrix solution procedure for three-dimensional panel methods

A new iterative matrix solution procedure for three-dimensional panel methods

By R. W. Clark