000 00419nam a22001217a 4500
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100 _aMauraca, Ralph J.
245 _aAerodynamics load distributions for the project fire configuration at mach numbers from .25 to 4.63 [NASA TN D-2604]
_cRalph J.Muraca
260 _aWashington, D. C.
_bNASA
300 _a28p
650 _aAerodynamic load distribution
942 _cREF
999 _c561292
_d561292