01310nam a2200313Ia 4500011446690MiAaHDL20141009010000.0m d cr bn ---auaua101115s1961 dcua bt f000 0 eng sdr-uiuc6408327(OCoLC)681379837UIUUIUUIUUNAS 1.15:X-502Gawienowski, John J.The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 /John, J. Gawienowski.Washington, D.C. :National Aeronautics and Space Administration,1961.23 p. :ill. ;26 cm.NASA technical memorandum ;X-502"March 1961."Cover title.Includes bibliographical references (p. 8).Full text also available online. Address as of 11/15/2010:http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660010440_1966010440.pdf.Mode of access: Internet.Wind tunnel testing.ConeAerodynamics.Boundary layer control.Ames Research Center.01144669020101115104816.020141009010000.020141112165512.02025-01-01T18:56:46Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6408327uiugSDRUIUCuiug.30112104504631UIU6408327UIUUIUC20250101googleuiug.301121045046311961pdbibUS fed doc