000			00500pam a2200145a 44500
040			_aP K Kelkar Library, IIT Kanpur
082			_aNASA _bCR-1926
100			_aGunness,C.
245	1		_aFLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS
260			_a _bNasa, Washington, D.C. _c1972
300			_a114
500			_aBound With Nasa Cr-1921-28
964			_gCIRC
997			_aTR8346 C
999			_c393017 _d393017