Add to ORKGA method for computing unsteady 2D aerodynamic coefficients is presented and its application helicopter main rotors and results are presented
Helicopter rotor blades encounter complex, time-varying changes in aerodynamic angle of attack, whic...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
Reduced-order aerodynamic models are tools that may be conveniently applied in a wide range of resea...
The steady aerodynamics characteristics of airfoils are represented by analytical formulas. Unsteady...
A semi-empirical mathematical model to compute steady and unsteady airfoil coefficients is presented...
A new comprehensive simulation tool for computation of the whole helicopter is currently being devel...
An unsteady panel method based on potential flow theory is developed for unsteady aerodynamic analys...
The paper presents the unsteady aerodynamic analysis of helicopter rotor with a panel method based o...
A robust unsteady rotor flowfield solver CLORNS code is established to predict the complex unsteady ...
AbstractA full-span free-wake method is coupled with an unsteady panel method to accurately predict ...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN024587 / BLDSC - British Library D...
AbstractThree-dimensional unsteady Euler equations are numerically solved to simulate the unsteady f...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
Communication to : 43rd AIAA aerospace sciences meeting and exhibit, Reno (USA), 10-13 janvier 2005S...
A 3-D unsteady panel method has been successfully used to predict the flow field around helicopter r...
Helicopter rotor blades encounter complex, time-varying changes in aerodynamic angle of attack, whic...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
Reduced-order aerodynamic models are tools that may be conveniently applied in a wide range of resea...
The steady aerodynamics characteristics of airfoils are represented by analytical formulas. Unsteady...
A semi-empirical mathematical model to compute steady and unsteady airfoil coefficients is presented...
A new comprehensive simulation tool for computation of the whole helicopter is currently being devel...
An unsteady panel method based on potential flow theory is developed for unsteady aerodynamic analys...
The paper presents the unsteady aerodynamic analysis of helicopter rotor with a panel method based o...
A robust unsteady rotor flowfield solver CLORNS code is established to predict the complex unsteady ...
AbstractA full-span free-wake method is coupled with an unsteady panel method to accurately predict ...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN024587 / BLDSC - British Library D...
AbstractThree-dimensional unsteady Euler equations are numerically solved to simulate the unsteady f...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
Communication to : 43rd AIAA aerospace sciences meeting and exhibit, Reno (USA), 10-13 janvier 2005S...
A 3-D unsteady panel method has been successfully used to predict the flow field around helicopter r...
Helicopter rotor blades encounter complex, time-varying changes in aerodynamic angle of attack, whic...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
Reduced-order aerodynamic models are tools that may be conveniently applied in a wide range of resea...