02098nam 2200517Ia 450 991069692450332120230902162259.0(CKB)5470000002383650(OCoLC)642326258(EXLCZ)99547000000238365020100618d2009 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierExperimental investigation of the application of microramp flow control to an oblique shock interaction[electronic resource] /Stefanie M. Hirt and Bernhard H. Anderson ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2009]1 online resource (27 pages) illustrationsNASA TM- ;2009-215630Title from title screen (viewed on June 17, 2010)."November 2009.""AIAA-2009-919."Includes bibliographical references (page 7).NASA technical memorandum ;2009-215630.Oblique shock wavesnasatBoundary layersnasatShock wave interactionnasatExperiment designnasatFactorial designnasatOblique shock waves.Boundary layers.Shock wave interaction.Experiment design.Factorial design.Hirt Stefanie M1386037Anderson Bernhard H1386038NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(47th :2009 :Orlando, Fla.)AIAA Aerospace Sciences Meeting.GPOGPOBOOK9910696924503321Experimental investigation of the application of microramp flow control to an oblique shock interaction3434603UNINA