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100 _aCrawford, Davis H.
245 1 _aNASA TN [D-118]
_bINVESTIGATION OF THE FLOW OVER A SPIKED-NOSE HEMISPHERE-CYLINDER AT A MACH NUMBER OF 6.8
_cDavis H. Crawford
260 _bNASA, Washington, D.C.
_c1959
300 _a59p
440 _aNASA Technical Note
500 _aNASA Technical Notes D-111-120 Bounded Volumes Accession No. 63636; Contents: TR 13094-102
650 _aAeronautics
942 _cTR
999 _c398322
_d398322