000			00515pam a2200133a 44500
082			_aNASA _bMEMO 4-20-59L
100			_aWornom,Dewey E
245	1		_aTRANSONIC AERODYNAMIC CHARACTURISTICS OF A 45DEGREE SWEPT-WING-FUSELAGE MODEL WITH A FINNED AND UNFINNED BODY PYLON-MOUNTED BENEATH THE FUSELAGE OR WING, INCLUDING MEASUREMENTS OF BODY LOADS
260			_a _bNasa, Washington, D.C. _c1959
300			_a57
500			_aBound With Nasa Memo 4-20-59l-4-30-59l Lack No.24-29
964			_gCIRC
997			_aTR7399 C
999			_c395615 _d395615