000			00523pam a2200145a 44500
082			_aNASA _bTR R-85
100			_aTrimpi,Robert L
245	1		_aA NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON
260			_a _bNasa, Washington, D.C. _c1961
300			_a55
500			_aBound With Nasa Tr R-81-84,86-90
700			_aCohen,Nathaniel B
964			_gCIRC
997			_aTR14358 C
999			_c398973 _d398973