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The Morphology of Flight Vehicles
Equations of Motion for Rigid Flight Vehicles
Introduction to Vehicle Aerodynamics
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aerodynamic aileron aircraft airfoil airloads airplane altitude angle of attack angular approximation assume atmosphere axes axis body body of revolution booster boundary condition calculated camber Chapter coefficient components compressor constant cruising damping derivatives determined differential dimensionless discussed drag dynamic engine entry equations of motion estimate Etkin fixed flight conditions flight path flight vehicle flow fluid force formula fuel function fuselage horizontal hypersonic inertial initial conditions inlet integral isentropic lift coefficient lifting surface linear loading longitudinal Mach number maneuver maximum mode mode shape normal orbit parameters perturbation phugoid pitching plane planform positive pressure problem propeller proportional propulsion quantities ramjet ratio reference rocket rotation Section sideslip slender-body theory solution specific impulse speed stability stability derivatives static streamlines subsonic supersonic theory thrust trajectory transonic trim turbojet typical variable vector velocity vertical weight wing zero