LEADER 02084nam  2200553Ia 450 
001 9910699736203321
005 20101202100951.0
035   $a(CKB)5470000002405586
035   $a(OCoLC)688609638
035   $a(EXLCZ)995470000002405586
100   $a20101202d1984      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes$b[electronic resource] /$fby H.T. Nagamatsu and R. E. Duffy
210  1$aTroy, N.Y. :$cRensselaer Polytechnic Institute,$d[1984]
215   $a1 online resource (iii, 39 pages) $cdigital, PDF file
225 1 $aNASA contractor report ;$v174667
300   $a"April 1984."
300   $a"Prepared for National Aeronautics and Space Administration, Lewis Research Center under grant no. NAS3-292."
320   $aIncludes bibliographical references (pages 36-39).
606   $aCircular cylinders$2nasat
606   $aGas turbines$2nasat
606   $aHeat flux$2nasat
606   $aHeat transfer$2nasat
606   $aHigh pressure$2nasat
606   $aPressure gradients$2nasat
606   $aShock tubes$2nasat
606   $aVanes$2nasat
615  7$aCircular cylinders.
615  7$aGas turbines.
615  7$aHeat flux.
615  7$aHeat transfer.
615  7$aHigh pressure.
615  7$aPressure gradients.
615  7$aShock tubes.
615  7$aVanes.
700   $aNagamatsu$b Henry T.$f-2006.$01413158
701   $aDuffy$b R. E$01413159
712 02$aRensselaer Polytechnic Institute.
712 02$aLewis Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699736203321
996   $aInvestigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes$93508856
997   $aUNINA