01017cam a2200253Ia 4500011427110MiAaHDL20141013010000.0m d cr bn ---auaua951212s1979 dcua b f000 0 eng dsdr-uiuc6368069(OCoLC)33892820BUFBUFABCOCLCGUIUUTL521.3.N18 no. 1452NAS 1.60:1452Smith, John M.(John Milton),1922-Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53 /John M. Smith.[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Office,1979.14 p. :ill. ;28 cm.NASA technical paper ;1452Includes bibliographical references.Mode of access: Internet.DiffusersAerodynamics.Gas-turbinesCombustion chambersTesting.TurbomachinesDiffusersTesting.01142711020101011112719.020141013010000.020141112173021.02025-01-02T19:04:29Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6368069uiugSDRUIUCuiug.30112106725085UIU6368069UIUUIUC20250102googleuiug.301121067250851979pdbibUS fed doc