000 00653nam a22001817a 4500
005 20200218115922.0
008 200218b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aTaylor, Robert T.
245 _aAn experimental investigation to determine the efffect of speed brake position on the longitudinal stability and trim of swept-Wing fighter airplane [NASA TN D-246]
_cRobert T. Taylor
260 _aWashingto, D. C.
_bNASA
_cFebruary 1960
300 _a46p
440 _aNational Aeronautics and Space Administration (NASA)
505 _aTEchnical note D-246
650 _aFighter airplane
942 _cREF
999 _c561370
_d561370