NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Inviscid modeling of aircraft trailing vorticesA survey is presented of inviscid theoretical methods that are useful in the study of lift-generated vortices. Concepts derived using these invisicid theories are cited which have helped to guide research directed at alleviating the velocities and rolling moments imposed on aircraft entering these wakes.
Document ID
19780004075
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rossow, V. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: Wake Vortex Minimization
Subject Category
Aerodynamics
Accession Number
78N12018
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19780004074Collected WorksWake Vortex Minimization
No Preview Available