01958nam 2200517 a 450 991069704180332120230902162120.0(CKB)5470000002384485(OCoLC)680065379(EXLCZ)99547000000238448520101109d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierUnified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields[electronic resource] /Gary E. EricksonHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2010]1 online resource (v, 32 pages) illustrationsNASA/TM- ;2010-216197Title from title screen (viewed on Nov. 9, 2010)."February 2010."Includes bibliographical references (pages 15-16)NASA technical memorandum ;216197.Aerodynamic configurationsnasatPressure sensitive paintsnasatFlow visualizationnasatShock wavesnasatStatic pressurenasatLeading edgesnasatAngle of attacknasatAerodynamic configurations.Pressure sensitive paints.Flow visualization.Shock waves.Static pressure.Leading edges.Angle of attack.Erickson Gary E1403144Langley Research Center.GPOGPOBOOK9910697041803321Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields3519400UNINA