000			00451pam a2200145a 44500
082			_aTR _bNACA-3036
100			_aMellenthin,Jack A.
245	1		_aTHE FLOW ABOUT A SECTION OF A FINITE-ASPECT-RATIO NACA 0015 AIRFOIL ON A TRANSONIC BUMP
260			_a _bNaca, Washington _c1953
300			_a30
440			_aNational Advisory Committee For Aeronautics-Tn-3036 _v
500			_aBound With: Naca-Tn-3031-3040
964			_gCIRC
997			_aTR3538 C
999			_c392231 _d392231