In addition to the Annotation of the forewords to the first and second edition, the translation encompasses sections of the monograph dealing with the theoretical flight dynamics of three dimensional maneuvers and the calculation of the trajectory of a winged rocket aircraft. Calculation equations are given for the cchandelle; only brief descriptions are given of the half roll, Immelmann, and roll. Extensive mathematical treatment of the behavior of a rocket powered winged vehicle in the atmosphere is presented from the point of view of the variational problem of the optimum flight program. (Author)
Flight Dynamics: Trajectories of Flight Vehicles (Selected Parts)
1970
34 pages
Report
No indication
English
Aeronautics , Rocket planes , Flight paths , Roll , Optimization , Lift , USSR , Translations
Flight Dynamics: Aircraft Trajectories
NTIS | 1966
|NTIS | 1970
|Flight dynamics of aeroelastic vehicles
NTRS | 1988
|Flight dynamics of aeroelastic vehicles
AIAA | 1988
|