01224cam a2200289I 4500011429062MiAaHDL20141009010000.0m d cr bn ---auaua840330s1967 dcua b f000 0 eng dsdr-uiuc6380438(OCoLC)10581258CLSengCLSOCLTXJOCLCQUIUUTL521.3.C6A3 no.908Agarwal, Urmila.Numerical investigation of unsteady laminar incompressible co-axial boundary layer flowsby Urmila Agarwal and T. Paul Torda. Prepared by Illinois Institute of Technology, Chicago, Ill., for Lewis Research Center.Washington,National Aeronautics and Space Administration;Springfield, Va.,For sale by the Clearinghouse for Federal Scientific and Technical Information,1967.xii, 122 p. :illus.NASA CR-908.Bibliography: p. 120-122.Mode of access: Internet.Nuclear rockets.Laminar flow.Boundary layer.Torda, T. Paul.United States.National Aeronautics and Space Administration.Lewis Research Center.Illinois Institute of Technology.01142906220101022101304.020141009010000.020141112164151.02026-01-18T19:26:33Z2026-01-18T18:30:03ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6380438uiugSDRUIUCuiug.30112106581165UIU6380438UIUUIUC20260118googleuiug.301121065811651967pdbibUS fed doc