02006oam 2200589I 450 991071667030332120210706140113.0(CKB)5470000002523461(OCoLC)23340598(OCoLC)761755645(EXLCZ)99547000000252346119910327j197210 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel measurements of surface-pressure fluctuations at Mach numbers of 1.6, 2.0, and 2.5 using 12 different transducers /by Thomas L. Lewis and Jules B. DodsWashington, D.C. :National Aeronautics and Space Administration,October 1972.1 online resource (49 pages) illustrationsNASA/TN ;D-7087"October 1972."Includes bibliographical references (pages 12-13).Aerodynamic noisenasatWind tunnel testsnasatWall pressure (Aerodynamics)MeasurementWind tunnel wallsAerodynamic noisefastWind tunnel wallsfastAerodynamic noise.Wind tunnel tests.Wall pressure (Aerodynamics)Measurement.Wind tunnel walls.Aerodynamic noise.Wind tunnel walls.Lewis Thomas L.1423293Dods Jules B.United States.National Aeronautics and Space Administration,Flight Research Center (U.S.)ABCABCAD#OCLCEOCLCQOCLCOOCLCQOCLCFCOPGPOBOOK9910716670303321Wind-tunnel measurements of surface-pressure fluctuations at Mach numbers of 1.6, 2.0, and 2.5 using 12 different transducers3550431UNINA