An entropy correction method for the unsteady full potential equation is presented. The unsteady potential equation is modified to account for entropy jumps across shock waves. The conservative form of the modified equation is solved in generalized coordinates using an implicit, approximate factorization method. A flux-biasing differencing method, which generates the proper amounts of artificial viscosity in supersonic regions, is used to discretize the flow equations in space. Comparisons between the present method and solutions of the Euler equations and between the present method and experimental data are presented. The comparisons show that the present method more accurately models solutions of the Euler equations and experiment than do...
We compare high-order methods including spectral difference (SD), flux reconstruction (FR), the entr...
A unified formulation is presented based on the full potential framework coupled with an appropriate...
The stability of curved or rectangular shocks in hypersonic inlets in reponse to flow perturbations ...
An entropy-correction method for the unsteady full potential equation is presented. The unsteady pot...
One of the most important uses of method that calculate unsteady aerodynamic loads is to predict and...
Aerodynamic methods for aeroelastic analysis are applied to various flow problems. These methods inc...
Modifications to unsteady transonic small disturbance theory to include entropy and vorticity effect...
A development was the time linearization of the density function. This linearization reduces the sol...
A theory to correct the transonic small disturbance (TSD) equation to treat strong shock waves in un...
The shock jump conditions for the Euler equations in their primitive form are derived by using gener...
We present a shock capturing method for unsteady laminar and turbulent flows. The proposed approach ...
1To avoid un-realistic solutions like expansion shocks from appearing as a part of a solution it is ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76175/1/AIAA-2007-4465-666.pd
Modifications that allow for more accurate modeling of flow fields when strong shocks are present we...
Properties of the shock relations for steady, irrotational, transonic flow are discussed and compare...
We compare high-order methods including spectral difference (SD), flux reconstruction (FR), the entr...
A unified formulation is presented based on the full potential framework coupled with an appropriate...
The stability of curved or rectangular shocks in hypersonic inlets in reponse to flow perturbations ...
An entropy-correction method for the unsteady full potential equation is presented. The unsteady pot...
One of the most important uses of method that calculate unsteady aerodynamic loads is to predict and...
Aerodynamic methods for aeroelastic analysis are applied to various flow problems. These methods inc...
Modifications to unsteady transonic small disturbance theory to include entropy and vorticity effect...
A development was the time linearization of the density function. This linearization reduces the sol...
A theory to correct the transonic small disturbance (TSD) equation to treat strong shock waves in un...
The shock jump conditions for the Euler equations in their primitive form are derived by using gener...
We present a shock capturing method for unsteady laminar and turbulent flows. The proposed approach ...
1To avoid un-realistic solutions like expansion shocks from appearing as a part of a solution it is ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76175/1/AIAA-2007-4465-666.pd
Modifications that allow for more accurate modeling of flow fields when strong shocks are present we...
Properties of the shock relations for steady, irrotational, transonic flow are discussed and compare...
We compare high-order methods including spectral difference (SD), flux reconstruction (FR), the entr...
A unified formulation is presented based on the full potential framework coupled with an appropriate...
The stability of curved or rectangular shocks in hypersonic inlets in reponse to flow perturbations ...