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060510s2003 |||a fr||||| |0 0|eng d |
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|a 1563475642
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|a 531.373.246
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|a Kimberlin, Ralph D.
|9 298692
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|a Flight testing of fixed-wing aircraft
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260 |
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|a Virginia :
|b American Institute of Aeronautics and Astronautics (AIAA),
|c 2003.
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300 |
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|a 441 p.
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440 |
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|a AIAA Education Series
|9 283011
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505 |
0 |
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|a Introduction;Methods for reducing data uncertainty in flight test data;Airspeed systems theory and calibration;Stall speed measurement;Determination of engine power in flight;propeller theory;Jet thrust measurement in flight;Level flight performance theory;Level flight performance flight test and data reduction methods for propeller-driven aircraft;Level flight performance jet aircraft;Range and endurance;Climb performance theory;Clim performance methods, data reduction, and expansion;Energy approach to performance flight;Turning performance;Methods for drag determination in flight;Airspeed vs flight path angle performance method for powered lift aircraft;Takeoff and landing theory and methods;Introduction to stability and control flight testing;Static longitudinal stability theory;Static longitudinal stability flight test method;Dynamic longitudinal stability theory;Dynamic longitudinal stability flight test methods and data reduction;Longitudinal maneuvering stability theory;Maneuvering stability methods and data;Longitudinal control and trim theory and flight test methods;Methods for improving longitudinal stability and control;Lateral-directional stability theory and flight test methods;Dynamic lateral-directional stability theory and flight test methods;Lateral control power (rolling performance);Directional control;Flying qualities;Stall characteristics;Airplane spin testing;Dive tresting for flutter, vibration an buffeting
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|a ENSAYOS DE VUELO
|9 298693
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|a MECANICA DE VUELO
|9 271009
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|a CONTROL DE VUELO
|9 282751
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1 |
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|a CARACTERISTICAS DE VUELO
|9 285254
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|a REGIMENES DE VUELO
|9 298694
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929 |
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|a COM FUN 2006
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942 |
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|c LIB
|6 _
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|a MON
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|a 19685
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|a Registro convertido en forma automatizada
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|a GEB
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|c 15825
|d 15825
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|a AR-LpUFI
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