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100   $a20230509c2018uuuu  -u-            -
101 0 $aeng
200 10$aNozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel
210   $aMoffett Field, California$cNational Aeronautics and Space Administration, Ames Research Center
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912   $a9910712254303321
996   $aNozzle plume$93291285
997   $aUNINA