NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Discrete-vortex model for the symmetric-vortex flow on conesA relatively simple but accurate potential flow model was developed for studying the symmetric vortex flow on cones. The model is a modified version of the model first developed by Bryson, in which discrete vortices and straight-line feeding sheets were used to represent the flow field. It differs, however, in the zero-force condition used to position the vortices and determine their circulation strengths. The Bryson model imposed the condition that the net force on the feeding sheets and discrete vortices must be zero. The proposed model satisfies this zero-force condition by having the vortices move as free vortices, at a velocity equal to at the local crossflow velocity at their centers. When the free-vortex assumption is made, a solution is obtained in the form of two nonlinear algebraic equations that relate the vortex center coordinates and vortex strengths to the cone angle and angle of attack. The vortex center locations calculated using the model are in good agreement with experimental values. The cone normal forces as well as center locations are in good agreement with the vortex cloud method of calculating symmetric flow fields.
Document ID
19900011630
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Gainer, Thomas G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
L-16586
NAS 1.60:2989
NASA-TP-2989
Accession Number
90N20946
Funding Number(s)
PROJECT: RTOP 505-60-21-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available