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008 100112s1986    it            000 0 ita d
035   $ab13868512-39ule_inst
040   $aDip.to Studi Giuridici$bita
100 1 $aVallone, Giancarlo$0241067
245 10$aAspetti giuridici e sociali nell'età aragonese :$bi Castriota in Terra d'Otranto /$cGiancarlo Vallone
260   $aGalatina :$bCongedo, 1986
300   $a211-264 p. ;$c24 cm.
500   $aEstr. da: Otranto 1480 : atti del Convegno internazionale di studio promosso in occasione del 5. centenario della caduta di Otranto ad opera dei turchi, Otranto, 19-23 maggio 1980 / a cura di Cosimo Damiano Fonseca
505 2 $gFascicolo rilegato in:$tMiscellanea : 1982-2008 / Giancarlo Vallone
650  4$aAlbanesi in Terra d'Otranto$xCastriota <famiglia>
650  4$aOtranto$xAssedio$x1480$aCongressi$y1980
907   $a.b13868512$b02-04-14$c12-01-10
912   $a991000513219707536
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996   $aAspetti giuridici e sociali nell'età aragonese$9230029
997   $aUNISALENTO
998   $ale027$b12-01-10$cm$da  $e-$fita$git $h0$i0

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101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$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
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801  2$bOCLCQ
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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