LEADER 00612nam  2200157z- 450 
001 9910712500403321
035   $a(CKB)5470000002493133
035   $a(EXLCZ)995470000002493133
100   $a20230509c2019uuuu  -u-            -
101 0 $aeng
200 10$aIndependent effects of Reynolds number and Mach number on aerodynamics of an iced swept wing
210   $aCleveland, Ohio$cNational Aeronautics and Space Administration, Glenn Research Center
906   $aBOOK
912   $a9910712500403321
996   $aIndependent effects of Reynolds number and Mach number on aerodynamics of an iced swept wing$93343572
997   $aUNINA