000			00502pam a2200145a 44500
082			_aTR _bCP-1298
100			_aIngle,G.
245	1		_aFLIGHT DETERMINATION OF THE RUDDER POWER AND DIRECTIONAL STABILITY OF THE FAIREY DELTA 2 AIRCRAFT USING A WINGTIP PARACHUTE
260			_a _bHer Majestys Stationery Office, London _c1974
300			_a21
440			_aAeronautical Research Council Current Papers _vCp No.1298
500			_aBound With: Arc Cp No.1291-1300
964			_gCIRC
997			_aTR3325 C
999			_c392380 _d392380