Add to ORKGAn explicit-implicit and an implicit two-dimensional Navier-Stokes code along with various grid generation capabilities were developed. A series of classical benckmark cases were simulated using these codes
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
The first objective was to analyze and design a true airspeed sensor which will replace the conventi...
Computational models which analyze viscous/inviscid flow processes in jet aircraft exhaust plumes ar...
A recently developed storm electrification model (SEM) is used to investigate the operating environm...
Statistical analysis of influencial aspects of wind profile disturbances design and dynamic response...
A generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics o...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
Video signal processing in low signal to noise environments - bandpass filter in multi-filter phase ...
Photoviscoelastic method for stress analysis of two dimensional viscoelastic model
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
A 35 km grid limited area mesoscale model was initialized with high density SESAME radiosonde data a...
Algorithms were developed for the extraction of two components of mean velocity, standard deviation,...
Space vehicle flight control modes for basic wind profiles - reduction of aerodynamic loads for wind...
STABCAR can be used to determine the characteristic roots of flexible, actively controlled aircraft,...
Laminar heating distributions were measured at hypersonic-hypervelocity flow conditions on a 1.9-per...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
The first objective was to analyze and design a true airspeed sensor which will replace the conventi...
Computational models which analyze viscous/inviscid flow processes in jet aircraft exhaust plumes ar...
A recently developed storm electrification model (SEM) is used to investigate the operating environm...
Statistical analysis of influencial aspects of wind profile disturbances design and dynamic response...
A generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics o...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
Video signal processing in low signal to noise environments - bandpass filter in multi-filter phase ...
Photoviscoelastic method for stress analysis of two dimensional viscoelastic model
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
A 35 km grid limited area mesoscale model was initialized with high density SESAME radiosonde data a...
Algorithms were developed for the extraction of two components of mean velocity, standard deviation,...
Space vehicle flight control modes for basic wind profiles - reduction of aerodynamic loads for wind...
STABCAR can be used to determine the characteristic roots of flexible, actively controlled aircraft,...
Laminar heating distributions were measured at hypersonic-hypervelocity flow conditions on a 1.9-per...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
The first objective was to analyze and design a true airspeed sensor which will replace the conventi...
Computational models which analyze viscous/inviscid flow processes in jet aircraft exhaust plumes ar...