01831nam 2200481 a 450 991070081200332120110927104033.0(CKB)5470000002412901(OCoLC)754813291(EXLCZ)99547000000241290120110927d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierConical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry[electronic resource] /Gregory C. Herring and James F. MeyersHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (29 pages) illustrations (some color)NASA/TM ;2011-217052Title from title screen (viewed on Sept. 27, 2011)."February 2011."Includes bibliographical references (pages 16-18).Conical shock strength determination on low sonic boom aircraft model by doppler global velocimetryVelocity measurementnasatSonic boomsnasatFlow characteristicsnasatSupersonic speednasatOblique shock wavesnasatVelocity measurement.Sonic booms.Flow characteristics.Supersonic speed.Oblique shock waves.Herring Gregory C1394410Meyers James F1405402Langley Research Center.GPOGPOBOOK9910700812003321Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry3504828UNINA