S. Shanks

发表

A three-dimensional incompressible Navier-Stokes flow solver using primitive variables

Dochan Kwak, Sukumar R. Chakravarthy, S. Chakravarthy, 1986 .

Aerodynamics of powered missile separation from a wing

J. Ahmad, S. Shanks, 1991 .

Flowfield predictions about lifting entry vehicles

G. Srinivasan, W. Nicolet, S. Shanks, 1982 .

Use of numerically generated body-fitted coordinate systems for solution of the Navier-Stokes equations

C. W. Mastin, S. P. Shanks, Joe F. Thompson, 1975 .

Viscous hypersonic flow over complex bodies at high angles of attack

W. Nicolet, S. Shanks, G. Srinivasan, 1984 .

Aerodynamics of powered missile separation from F/A-18 aircraft

P. G. Buning, J. U. Ahmad, S. P. Shanks, 1993 .

An incompressible Navier-Stokes flow solver in three-dimensional curvilinear coordinate systems using primitive variables

D. Kwak, S. R. Chakravarthy, S. P. Shanks, 1984 .

Solutions of the navier-stokes equations in various flow regimes on fields containing any number of arbitrary bodies using boundary-fitted coordinate systems

Joe F. Thompson, F. Thames, C. Mastin, 1976 .

Numerical Solution of Three-Dimensional Navier-Stokes Equations Showing Trailing Tip Vortices

S. Shanks, Joe F. Thompson, J. C. Wu, 1974 .