Static and Dynamic Testing of Blunt Bodies in a Subsonic Magnetic Suspension Wind TunnelThe MIT 6-inch magnetic suspension wind tunnel is used in two configurations to measure lift forces of two blunt bodies and produce free-to-pitch oscillations driven by capsule static stability and dynamic instabilities. Lift tests show that static aerodynamic data can be measured on a magnetically levitated model without moment control. Free-to- oscillate results show that magnetic suspension balance system (MSBS) can produce capsule dynamics suitable for extracting static and dynamic stability data.
Document ID
20190033957
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Schoenenberger, Mark (NASA Langley Research Center Hampton, VA, United States)
Finke, Colton (Texas A&M Univ. College Station, TX, United States)
Britcher, Colin (Old Dominion Univ. Norfolk, VA, United States)
Cox, David (NASA Langley Research Center Hampton, VA, United States)
Schott, Timothy (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
December 16, 2019
Publication Date
November 7, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-30952Report Number: NF1676L-30952
Meeting Information
Meeting: International Conference on Flow Dynamics