000			01378cam a2200337 a 4500
001			7049296C5098
003			COMPanion
008			190723b xx || |000 ||eng
020			_a188488542X
040			_aUNAQ _bspa _cUNAQ
082			_a629.134 R67
100			_aRoskam, Jan Dr. _94966
245			_aAirplane Design _cDr. Jan Roskam.
250			_a3a ed.
264			_aEstados Unidos _bDAR corporation _c2003.
300			_a207 p. _bil. _c28 cm.
490			_aRoskam
500			_aContiene índice.
505	0		_aParte I: Preliminary sizing of airplanes (2003)
505			_aParte II: Preliminary configuration design and integration of the propulsion system (1997)
505			_aParte III: Layout design of cockpit, fuselage, wing and empennage: cutaways and inboard profiles(2002).
505			_aPart IV: Layout of landing gear and systems(2000).
505			_aParte V: Component weight estimation (2003).
505			_aParte VI: Preliminary calculation of aerodynamic, thrust and power characteristics (2000).
505			_aParte VII: Determination of stability, control and performance characteristics: FAR and military requirements (2002).
505			_aParte VII: Airplane cost estimation: design, development,manufacturing and operating (2002).
520			_aBK
521			_a191
650		4	_aDiseño - _vAviones _919932
999			_c11690 _d11690