Add to ORKGA vortex lattice method has been developed to analyse simple, swept, tapered wings with spanta ise segmented flaps at both leading and trailing edges . Classical planar horse shoe vortex is used as the basic solution to the governing Laplace's equation . Compressibility corrections (ire accounted for using Prandil-Glauert analogy modified as applicable to wins with deflected flaps. Extensive numerical experimentation has been carried to detcrinine the optin/um lattice layout. The method has been validated using a number of test cases available in published literatur
A generalized vortex lattice method for complex lifting surfaces with flap and aileron deflection is...
Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, t...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
A method and a computer program in FORTRAN have been developed for the analysis of wings with segmen...
A method and a computer program in FORTRAN have been developed for the analysis of wings with segmen...
A nonplanar vortex lattice method is described for calculating the potential flow aerodynamic charac...
A nonplanar vortex lattice method is described for calculating the potential flow aerodynamic charac...
An important problem of analysis of complex wing planforms with multisegmented is addressed. Nonplan...
An important problem of analysis of complex wing planforms with multisegmented is addressed. Nonplan...
A generalized vortex lattice method for complex lifting surfaces with flap and aileron deflection is...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
Flapping flight is an increasingly popular area of research, with applications to micro-unmanned ai...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
peer reviewedFlapping flight is an increasingly popular area of research, with applications to micro...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
A generalized vortex lattice method for complex lifting surfaces with flap and aileron deflection is...
Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, t...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
A method and a computer program in FORTRAN have been developed for the analysis of wings with segmen...
A method and a computer program in FORTRAN have been developed for the analysis of wings with segmen...
A nonplanar vortex lattice method is described for calculating the potential flow aerodynamic charac...
A nonplanar vortex lattice method is described for calculating the potential flow aerodynamic charac...
An important problem of analysis of complex wing planforms with multisegmented is addressed. Nonplan...
An important problem of analysis of complex wing planforms with multisegmented is addressed. Nonplan...
A generalized vortex lattice method for complex lifting surfaces with flap and aileron deflection is...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
Flapping flight is an increasingly popular area of research, with applications to micro-unmanned ai...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
peer reviewedFlapping flight is an increasingly popular area of research, with applications to micro...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
A generalized vortex lattice method for complex lifting surfaces with flap and aileron deflection is...
Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, t...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...