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Potential benefits of magnetic suspension and balance systemsThe potential of Magnetic Suspension and Balance Systems (MSBS) to improve conventional wind tunnel testing techniques is discussed. Topics include: elimination of model geometry distortion and support interference to improve the measurement accuracy of aerodynamic coefficients; removal of testing restrictions due to supports; improved dynamic stability data; and stores separation testing. Substantial increases in wind tunnel productivity are anticipated due to the coalescence of these improvements. Specific improvements in testing methods for missiles, helicopters, fighter aircraft, twin fuselage transports and bombers, state separation, water tunnels, and automobiles are also forecast. In a more speculative vein, new wind tunnel test techniques are envisioned as a result of applying MSBS, including free-flight computer trajectories in the test section, pilot-in-the-loop and designer-in-the-loop testing, shipboard missile launch simulation, and optimization of hybrid hypersonic configurations. Also addressed are potential applications of MSBS to such diverse technologies as medical research and practice, industrial robotics, space weaponry, and ore processing in space.
Document ID
19870008285
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lawing, Pierce L.
(NASA Langley Research Center Hampton, VA, United States)
Dress, David A.
(NASA Langley Research Center Hampton, VA, United States)
Kilgore, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:89079
NASA-TM-89079
Report Number: NAS 1.15:89079
Report Number: NASA-TM-89079
Accession Number
87N17718
Funding Number(s)
PROJECT: RTOP 505-61-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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