Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76476/1/AIAA-1990-603-194.pd
Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of ...
A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interaction...
A numerical procedure was developed to compute the inviscid super/hypersonic flow fields about compl...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76211/1/AIAA-10846-311.pd
Aerodynamic forces are obtained for laminar flow past a slender wedge at high Mach number and high R...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
The construction of a reliable, shock capturing finite difference method to solve the Euler equation...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
AbstractThis paper deals with the numerical solution of inviscid compressible flows. The three-dimen...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76052/1/AIAA-12372-854.pd
A numerical procedure has been developed to compute the inviscid super/hypersonic flow field about c...
A new technique is described for solving supersonic fluid dynamics problems containing multiple regi...
The Advection Upstream Splitting Method (AUSM) is used to compute 2D inviscid hypersonic flow over a...
An approximate solution technique was developed for 3-D inviscid, hypersonic flows. The method emplo...
Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of ...
A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interaction...
A numerical procedure was developed to compute the inviscid super/hypersonic flow fields about compl...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76211/1/AIAA-10846-311.pd
Aerodynamic forces are obtained for laminar flow past a slender wedge at high Mach number and high R...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
The construction of a reliable, shock capturing finite difference method to solve the Euler equation...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
AbstractThis paper deals with the numerical solution of inviscid compressible flows. The three-dimen...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76052/1/AIAA-12372-854.pd
A numerical procedure has been developed to compute the inviscid super/hypersonic flow field about c...
A new technique is described for solving supersonic fluid dynamics problems containing multiple regi...
The Advection Upstream Splitting Method (AUSM) is used to compute 2D inviscid hypersonic flow over a...
An approximate solution technique was developed for 3-D inviscid, hypersonic flows. The method emplo...
Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of ...
A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interaction...
A numerical procedure was developed to compute the inviscid super/hypersonic flow fields about compl...
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