000			00427pam a2200133a 44500
082			_aNASA _bTN D-1380
100			_aYoung,Lou S
245	1		_aEFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0
260			_a _bNasa, Washington, D.C. _c1962
300			_a23
500			_aBound With Nasa Tn D-1376-79
964			_gCIRC
997			_aTR12901 C
999			_c397522 _d397522