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panel method (fluid dynamics)

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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 Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination By D. J. Strash

Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination

Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination

By D. J. Strash

View Development of multiobjective optimization techniques for sonic boom minimization By Aditi Chattopadhyay

Development of multiobjective optimization techniques for sonic boom minimization

Development of multiobjective optimization techniques for sonic boom minimization

By Aditi Chattopadhyay

View Performance analysis of three dimensional integral equation computations on a massively parallel computer By Terry G. Logan

Performance analysis of three dimensional integral equation computations on a massively parallel computer

Performance analysis of three dimensional integral equation computations on a massively parallel computer

By Terry G. Logan

View User's guide to PANCOR By William B. Kemp

User's guide to PANCOR

User's guide to PANCOR

By William B. Kemp

View Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems By A. Hamed

Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems

Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems

By A. Hamed

View The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis By Qiangang Liu

The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis

The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis

By Qiangang Liu

View An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application By H. W. M. Hoeijmakers

An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application

An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application

By H. W. M. Hoeijmakers

View TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations By

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

By

View Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model By Zachary T. Applin

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

By Zachary T. Applin

View Steady and unsteady three-dimensional transonic flow computations by integral equation method By Hung Hu

Steady and unsteady three-dimensional transonic flow computations by integral equation method

Steady and unsteady three-dimensional transonic flow computations by integral equation method

By Hung Hu

View USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics By Michael R. Wiese

USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics

USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics

By Michael R. Wiese

View Hypersonic vehicle simulation model By

Hypersonic vehicle simulation model

Hypersonic vehicle simulation model

By

View TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations By

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

By

View Numerical approach for the aerodynamic analysis of airfoils with laminar separation By David W. Halt

Numerical approach for the aerodynamic analysis of airfoils with laminar separation

Numerical approach for the aerodynamic analysis of airfoils with laminar separation

By David W. Halt

View A numerical analysis applied to high angle of attack three-dimensional inlets By Danny P. Hwang

A numerical analysis applied to high angle of attack three-dimensional inlets

A numerical analysis applied to high angle of attack three-dimensional inlets

By Danny P. Hwang

View Study of the mutual interaction between a wing wake and an encountering airplane By A. B. Walden

Study of the mutual interaction between a wing wake and an encountering airplane

Study of the mutual interaction between a wing wake and an encountering airplane

By A. B. Walden

View A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies By M. H. L. Hounjet

A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies

A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies

By M. H. L. Hounjet

View Study of the integration of wind tunnel and computational methods for aerodynamic configurations By Lindsay E. Browne

Study of the integration of wind tunnel and computational methods for aerodynamic configurations

Study of the integration of wind tunnel and computational methods for aerodynamic configurations

By Lindsay E. Browne