000			00437pam a2200133a 44500
082			_aNASA _bTM X-26 -
100			_aSpreemann,Kenneth P
245	1		_aDESIGN GUIDE FOR PITCH-UP EVALUATIO AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS
260			_a _bNasa, Washington, D.C. _c1959
300			_a37
500			_aBound With Nasa Tm X-22-39
964			_gCIRC
997			_aTR9327 C
999			_c394533 _d394533