000 00601nam a2200169 4500
005 20200527153222.0
008 200527b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
082 _aNACA
_bTN-2882
100 _aStokes, Fred H.
245 _aTheoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
_cFred, H. Stokes and J. T. Matthews
260 _aWashington, D. C.
_bNational Advisory Committee for Aeronautics
_c1953
300 _a41p
700 _aMatthews, J. T.
942 _cBK
999 _c562474
_d562474