The roll-up of a vortex sheet is analyzed by two approaches. The first is based on exact compressible Euler equations while the second is based on the exact incompressible Navier-Stokes equations. The inviscid calculations for the two-dimensional problem do not indicate any roll-up of the sheet. On the other hand, the viscous calculations capture the dynamics of the roll-up rather well. This suggests that the generally held views regarding the roll-up process of aircraft wakes, namely, that it be treated as an inviscid process, may not be completely accurate
Aircraft trailing vortices constitute both a kaleidoscope of instructive fluid dynamics phenomena a...
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77273/1/AIAA-1992-409-534.pd
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
A simple form is presented of the relationships for the inviscid, fully developed structure of lift-...
Simplified models of the vortex distribution over cylindrical surfaces are developed. The effect of ...
The dynamic interaction of aircraft wake vortices was investigated using both inviscid and viscous m...
In January 1991, one of us (JNH) published a report [1] that proposed alternative strategies for the...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
This paper addresses a discrepancy found between the rate of roll-up of a trailing vortex sheet calc...
The Betz conjecture, its extensions and applications, regarding the final rolled-up structure of a v...
Flight tests were conducted to verify the results found in ground base facilities of the effect of s...
Measurements were made in the NASA-Ames 40- by 80-foot wind tunnel of the rolling moment induced on ...
Aircraft trailing vortices constitute both a kaleidoscope of instructive fluid dynamics phenomena a...
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77273/1/AIAA-1992-409-534.pd
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
A simple form is presented of the relationships for the inviscid, fully developed structure of lift-...
Simplified models of the vortex distribution over cylindrical surfaces are developed. The effect of ...
The dynamic interaction of aircraft wake vortices was investigated using both inviscid and viscous m...
In January 1991, one of us (JNH) published a report [1] that proposed alternative strategies for the...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
This paper addresses a discrepancy found between the rate of roll-up of a trailing vortex sheet calc...
The Betz conjecture, its extensions and applications, regarding the final rolled-up structure of a v...
Flight tests were conducted to verify the results found in ground base facilities of the effect of s...
Measurements were made in the NASA-Ames 40- by 80-foot wind tunnel of the rolling moment induced on ...
Aircraft trailing vortices constitute both a kaleidoscope of instructive fluid dynamics phenomena a...
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...