000			00425pam a2200145a 44500
082			_aTR _bCOA-14
100			_aNonweiler,T.
245	1		_aWAVE DRAG OF HIGHLY SEWPT WINGS _cA COMPARISON OF LINEAR THEORY AND SLENDER BODY THEORY
260			_a _bCollege Of Aeronautics, Cranfield _c1954
300			_a14
440			_aCollege Of Aeronautics _vNo.14
500			_aBound With: Coa 5-65
964			_gCIRC
997			_aTR3023 C
999			_c392733 _d392733