000			00554pam a2200133a 44500
082			_aNASA _bMEMO 1-22-59L
100			_aBoisseau,Peter C
245	1		_aLOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES
260			_a _bNasa, Washington, D.C. _c1959
300			_a25
500			_aBound With Nasa Memo 1-15-59l-20,23-31 Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
964			_gCIRC
997			_aTR17736 C
999			_c401952 _d401952