000			00485pam a2200145a 44500
082			_aNASA _bTN D-7097
100			_aSorrells,Russell B
245	1		_aNUMERICAL METHOD FOR DESIGN OF MINIMUM-DRAG SUPERSONIC WING CAMBER WITH CONSTRAINTS ON PITCHING MOMENT AND SUFACE DEFORMATION.
260			_a _bNasa, Washington, D.C. _c1972
300			_a47
500			_aBound With Nasa Tn D_7090-7096,7098-7099.Lack No-7094.
700			_aMiller,David S
964			_gCIRC
997			_aTR14396 C
999			_c399048 _d399048