Duncan, W. J.  <br/><br/>
Control and stability of aircraft /  
W. J. Duncan 
 - Cambridge :   John Wright & Sons Ltd.,   1952,   1959 
 - 384 p. 
<br/><br/>Introductory survey - Elementary machanics of flight - The equations of motion of rigid aircraft - Methods for solving the dynamical equations and for investigating stability - Longitudinal-symmetric motion - Lateral-antisymmetric motion - Flat controls in general - The measurement of aerodynamic derivatives - Controls for roll, pitch and yaw - Static stability - Stalling and the spin - The influence of distortion of the structure - The influence of the compressibility of the air - Flaps for landing and take-off - Sundry topics 
<br/><br/><label>Subjects--Topical Terms: </label><br/>AERODINAMICA<br/>MECANICA DE VUELO<br/>ESTABILIDAD LONGITUDINAL<br/>ESTABILIDAD LATERAL<br/>FLAPS<br/>MEDICIONES EN AERODINAMICA<br/>ESTABILIDAD ESTATICA<br/>DISTORSION DE ESTRUCTURA<br/>COMPRESIBILIDAD<br/>ESTABILIDAD Y CONTROL
<br/><br/><label>Universal Decimal Class. No.: </label>531.373.2-537