000 00627nam a22001817a 4500
003 OSt
005 20220912115726.0
008 220912b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
245 _aNASA TN [D-11]
_bmeasured and predicted section wave drag coefficients at a mach number of 1.6 for a delta a wing with two airfoll sections
_cFrederick C. Grant
260 _aWashington
_bNational Aeronautics and Space Administration
_c1959
300 _a41p
440 _aNASA Technical Note
500 _aTechnical Reports D-11-20 Bound Vol. No.63343
650 _aAerodynamics
942 _cTR
999 _c566111
_d566111