Add to ORKGThe inviscid flow past a BGK-1, NACA0012 amp; NACA0006 airfoils at a few subsonc Mach numbers amp; incidence, is computed by twe Full Potential Codes - one developed in this Divsiion which is an improvement over the basic code developed by Le Carlson (NAL SOF 0008) amp; the other. a BGKcode, (NAL SOF 0005) and the Euler code, for the 'free air' case and compared. An assessment of the capabilities of these codes, the computing times amp; hence, their appropriateness for any particular case as defined by the airfoil, Mach number and incidence, is made in this stud
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out ...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The inviscid flow past a BGK-1, NACA0012 amp; NACA0006 airfoils at a few subsonc Mach numbers amp; i...
The inviscid flow over a Williams two element airfoil (configuration A) is computed using an Euler c...
The application of potential-flow theory together with boundary-layer theory to airfoil design and a...
A quantitative comparison between the Euler and full potential formulations with respect to speed an...
Several numerical methods exist for solving two-dimensional transonic full potential equations, appe...
Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out ...
An implicit central difference code is used to calculate two-dimensional inviscid and thin-layer Nav...
Low Mach number viscous-inviscid interaction is considered using panel methods, direct and inverse b...
Full-potential, Euler, and Navier-Stokes computational fluid dynamics (CFD) codes were evaluated for...
Under the framework of the DLG-CAE cooperation topic: 92-16, numerical investigation is carried out ...
Computational expedience and adequate predictive accuracy for certain engineering applications, make...
Two time accurate schemes for the solution of Euler equations are presented: an explicit residual av...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out ...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The inviscid flow past a BGK-1, NACA0012 amp; NACA0006 airfoils at a few subsonc Mach numbers amp; i...
The inviscid flow over a Williams two element airfoil (configuration A) is computed using an Euler c...
The application of potential-flow theory together with boundary-layer theory to airfoil design and a...
A quantitative comparison between the Euler and full potential formulations with respect to speed an...
Several numerical methods exist for solving two-dimensional transonic full potential equations, appe...
Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out ...
An implicit central difference code is used to calculate two-dimensional inviscid and thin-layer Nav...
Low Mach number viscous-inviscid interaction is considered using panel methods, direct and inverse b...
Full-potential, Euler, and Navier-Stokes computational fluid dynamics (CFD) codes were evaluated for...
Under the framework of the DLG-CAE cooperation topic: 92-16, numerical investigation is carried out ...
Computational expedience and adequate predictive accuracy for certain engineering applications, make...
Two time accurate schemes for the solution of Euler equations are presented: an explicit residual av...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out ...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...