000			00508pam a2200145a 44500
082			_aNACA _bTN 3789
100			_aEdwards,G G,Dickson,J K
245	1		_aTHE RESULTS OF WIND-TUNNEL TESTS TO A MACH NUMBER OF 0.90 OF A FOUR-ENGINE PROPELLER-DRIVEN AIRPLANE CONFIGURATION HAVING A WING WITH 40 DEGREE OF SWEEPBACK AND AN ASPECT RATIO OF 10
260			_a _bNaca, Washington _c1956
300			_a171
500			_aBound With Naca Tn 3780-88.
700			_aSutton,F B
964			_gCIRC
997			_aTR11267 C
999			_c396750 _d396750