000			00477pam a2200145a 44500
082			_aNACA _bTN 3134
100			_aGates,Ordway B
245	1		_aA METHOD FOR ESTIMATING VARIATIONS TN THE ROOTS OF THE LATERAL-STABILITY QUARTIC DUE TO CHANGES IN MASS AND AERODYNAMIC OPARAMETERS OF AN AIRPLANE.
260			_a _bNaca, Washington _c1954
300			_a66
500			_aBound With Naca Tn-3130-3133,3135-3139.
700			_aWoodling,C H
964			_gCIRC
997			_aTR15307 C
999			_c399737 _d399737