000 00635 a2200157 4500
005 20221125103424.0
100 _aHenderson, Arthur
245 _aNASA TN [D-819]
_bCharts for conical and two-dimensinal onlique-shock flow parameters in helium at mach numbers from about 1 to 100
_cArthur Henderson and Dorothy O. Braswell
260 _aWashington
_bNational Aeronautics and Space Administration
_c1961
300 _a185p
440 _aNASA Technical Note
500 _aNASA Technical Note D-811-20 Bounded Volumes Accession No. 65482; Contents: TR7492-7500
650 _aAeronautics
700 _aBraswell,Dorothy O.
942 _cTR
999 _c566290
_d566290