000			00519pam a2200133a 44500
082			_aNASA _bTM X-183
100			_aYates,E Carson
245	1		_aUSE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT OR UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS
260			_a _bNasa, Washington, D.C. _c1960
300			_a51
500			_aBound With Nasa Tm X-182,186-97 Lack No.184-85,187-90,192,194,196
964			_gCIRC
997			_aTR13579 C
999			_c399248 _d399248