Design, Calibration, And Performance Of A Tandem Sting Support System With Offset Balances For High Speed Testing
US Air Force T & E Days ; 2008 ; Los Angeles, CA
01.01.2008
13 pages
Aufsatz (Konferenz)
Englisch
Aeronautics , Astronautics , AIAA , Air force , US air force
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Improved drag element for wind tunnel sting balances
AIAA | 1985
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