LEADER 02089nam  2200565I  450 
001 9910702659303321
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035   $a(CKB)5470000002429595
035   $a(OCoLC)897221241
035   $a(DGPO)000936138
035   $a(EXLCZ)995470000002429595
100   $a20141202j201405    ua         0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel $etheory and experiment /$fBenjamin D. Goldman, Robert C. Scott, Earl H. Dowell
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 2014.
215   $a1 online resource (44 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218267
300   $aTitle from title screen (viewed Dec. 1, 2014).
300   $a"May 2014."
320   $aIncludes bibliographical references (pages 43-44).
517   $aNonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel 
606   $aThermal protection$2nasat
606   $aAerodynamic brakes$2nasat
606   $aAeroelasticity$2nasat
606   $aHeat shielding$2nasat
606   $aInflatable structures$2nasat
606   $aHigh temperature tests$2nasat
606   $aFlutter$2nasat
615  7$aThermal protection.
615  7$aAerodynamic brakes.
615  7$aAeroelasticity.
615  7$aHeat shielding.
615  7$aInflatable structures.
615  7$aHigh temperature tests.
615  7$aFlutter.
700   $aGoldman$b Benjamin D.$01422814
702   $aScott$b Robert C.
702   $aDowell$b E. H.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702659303321
996   $aNonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel$93548364
997   $aUNINA