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An efficient algorithm using matrix methods to solve wind tunnel force-balance equationsAn iterative procedure applying matrix methods to accomplish an efficient algorithm for automatic computer reduction of wind-tunnel force-balance data has been developed. Balance equations are expressed in a matrix form that is convenient for storing balance sensitivities and interaction coefficient values for online or offline batch data reduction. The convergence of the iterative values to a unique solution of this system of equations is investigated, and it is shown that for balances which satisfy the criteria discussed, this type of solution does occur. Methods for making sensitivity adjustments and initial load effect considerations in wind-tunnel applications are also discussed, and the logic for determining the convergence accuracy limits for the iterative solution is given. This more efficient data reduction program is compared with the technique presently in use at the NASA Langley Research Center, and computational times on the order of one-third or less are demonstrated by use of this new program.
Document ID
19720019352
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smith, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-6860
L-8278
Report Number: NASA-TN-D-6860
Report Number: L-8278
Accession Number
72N27002
Funding Number(s)
PROJECT: RTOP 501-06-10-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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