000			00433pam a2200133a 44500
082			_aNASA _bTN D-4929
100			_aQueijo,M J
245	1		_aTHEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW
260			_a _bNasa, Washington, D.C. _c1968
300			_a76
500			_aBound With Nasa Tn D-4921-28, 4930.
964			_gCIRC
997			_aTR12449 C
999			_c397146 _d397146