000			00467pam a2200133a 44500
082			_aNASA _bMEMO 5-26-59L
100			_aGainer,Patrick A
245	1		_aMODIFIED MATRIX METHOD FOR CALCULATING STEADY-STATE SPAN LODING ON FLEXIBLE WINGS IN SUBSONIC FLIGHT
260			_a _bNasa, Washington, D.C. _c1959
500			_aBound With Nasa Memo 5-12-59l-5-25-59l And 5-28-59l Lack No.14-17, 19, 21-22, 27
700			_aAiken,William S
964			_gCIRC
997			_aTR7411 C
999			_c402220 _d402220