000			00487pam a2200145a 44500
082			_aNASA _bTN D-398
100			_aLlewellyn,Charles P
245	1		_aEFFECT OF REYNOLDS NUMBER ON THE LATERAL-STABILITY DERIVATIVES AT LOW SPEED OF SWEPTBACK- AND DELTA-WING-FUSELAGE COMBINATIONS OSCILLATING IN YAW
260			_a _bNasa, Washington, D.C. _c1960
300			_a45
500			_aBound With Nasa Tn D-391-97,399-400
700			_aWolhart,Walter D
964			_gCIRC
997			_aTR15931 C
999			_c400474 _d400474