01852oam 2200517 450 991070614540332120170906104328.0(CKB)5470000002454974(OCoLC)858269523(EXLCZ)99547000000245497420130912j199908 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierStatic performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control /Scott C. Asbury and Craig A. HunterHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,August 1999.1 online resource (134 pages) illustrationsNASA/TM ;1999-209513"August 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 19-20).Exhaust nozzlesnasatPorositynasatHole geometry (mechanics)nasatCavitiesnasatThrust vector controlnasatExhaust nozzles.Porosity.Hole geometry (mechanics)Cavities.Thrust vector control.Asbury Scott C.1397878Hunter Craig A(Craig Allen),Langley Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706145403321Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control3549351UNINA