LEADER 02006oam  2200589I  450 
001 9910716670303321
005 20210706140113.0
035   $a(CKB)5470000002523461
035   $a(OCoLC)23340598$z(OCoLC)761755645
035   $a(EXLCZ)995470000002523461
100   $a19910327j197210    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel measurements of surface-pressure fluctuations at Mach numbers of 1.6, 2.0, and 2.5 using 12 different transducers /$fby Thomas L. Lewis and Jules B. Dods
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1972.
215   $a1 online resource (49 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7087
300   $a"October 1972."
320   $aIncludes bibliographical references (pages 12-13).
606   $aAerodynamic noise$2nasat
606   $aWind tunnel tests$2nasat
606   $aWall pressure (Aerodynamics)$xMeasurement
606   $aWind tunnel walls
606   $aAerodynamic noise$2fast
606   $aWind tunnel walls$2fast
615  7$aAerodynamic noise.
615  7$aWind tunnel tests.
615  0$aWall pressure (Aerodynamics)$xMeasurement.
615  0$aWind tunnel walls.
615  7$aAerodynamic noise.
615  7$aWind tunnel walls.
700   $aLewis$b Thomas L.$01423293
702   $aDods$b Jules B.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aFlight Research Center (U.S.)
801  0$bABC
801  1$bABC
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910716670303321
996   $aWind-tunnel measurements of surface-pressure fluctuations at Mach numbers of 1.6, 2.0, and 2.5 using 12 different transducers$93550431
997   $aUNINA