000			00448pam a2200145a 44500
082			_aNASA _bMEMO 4-3-59L -
100			_aMargolis,Kenneth
245	1		_aFORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS
260			_a _bNasa, Washington, D.C. _c1959
300			_a26
500			_aBound With Nasa Memo 4-1-59l-4-19-59l
700			_aElliott,Miriam H
964			_gCIRC
997			_aTR7688 C
999			_c393201 _d393201