Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77273/1/AIAA-1992-409-534.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83577/1/AIAA-2010-2707-714.pd
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
The interaction of jets, wakes, and vortices on lifting bodies represents a broad spectrum of aerody...
This is the published version. Copyright © 2012 American Institute of PhysicsA two-dimensional nume...
The results of an experimental investigation into aircraft vortex wakes are presented. The main aims...
The ability of the Vortex Separation AEROdynamics (VSAERO) program to calculate aerodynamic loads on...
The study reported here was initiated by observations of condensation trails that occur behind trans...
A research on studying the effect of the wake generated by an aircraft wing section on a following a...
The roll-up of a vortex sheet is analyzed by two approaches. The first is based on exact compressibl...
The objective of this dissertation research is to develop a surface vorticity method for simulating ...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
A method for predicting aerodynamic characteristics of slender wings with edge vortex separation was...
A simple form is presented of the relationships for the inviscid, fully developed structure of lift-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83577/1/AIAA-2010-2707-714.pd
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
The interaction of jets, wakes, and vortices on lifting bodies represents a broad spectrum of aerody...
This is the published version. Copyright © 2012 American Institute of PhysicsA two-dimensional nume...
The results of an experimental investigation into aircraft vortex wakes are presented. The main aims...
The ability of the Vortex Separation AEROdynamics (VSAERO) program to calculate aerodynamic loads on...
The study reported here was initiated by observations of condensation trails that occur behind trans...
A research on studying the effect of the wake generated by an aircraft wing section on a following a...
The roll-up of a vortex sheet is analyzed by two approaches. The first is based on exact compressibl...
The objective of this dissertation research is to develop a surface vorticity method for simulating ...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
A method for predicting aerodynamic characteristics of slender wings with edge vortex separation was...
A simple form is presented of the relationships for the inviscid, fully developed structure of lift-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83577/1/AIAA-2010-2707-714.pd
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
DOI
Add to ORKG