000			00548pam a2200157a 44500
005			20180906155109.0
008			180906b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
100			_aWest, F. E.
245	1		_aEffects of body-mounted lateral controls and speed brakers the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.90. [NASA TN D-522]
260			_aNASA _bWashington, D.C. _c1960
300			_avarious pagings
500			_aBound With NASA TN D-521,523-530.
942			_cTR
999			_c399483 _d399483