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Development of test methods for scale model simulation of aerial applications in the NASA Langley Vortex Research FacilityAs part of basic research to improve aerial applications technology, methods were developed at the Langley Vortex Research Facility to simulate and measure deposition patterns of aerially-applied sprays and granular materials by means of tests with small-scale models of agricultural aircraft and dynamically-scaled test particles. Interactions between the aircraft wake and the dispersed particles are being studied with the objective of modifying wake characteristics and dispersal techniques to increase swath width, improve deposition pattern uniformity, and minimize drift. The particle scaling analysis, test methods for particle dispersal from the model aircraft, visualization of particle trajectories, and measurement and computer analysis of test deposition patterns are described. An experimental validation of the scaling analysis and test results that indicate improved control of chemical drift by use of winglets are presented to demonstrate test methods.
Document ID
19800015768
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jordan, F. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1980
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-81805
Report Number: NASA-TM-81805
Meeting Information
Meeting: AIAA 11th Aerodyn. Testing Conf.
Location: Colorado Springs, CO
Country: United States
Start Date: March 18, 1980
End Date: March 20, 1980
Accession Number
80N24260
Funding Number(s)
PROJECT: RTOP 505-41-83-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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