Engineering Analysis of Flight Vehicles

aerodynamic aileron aircraft airfoil airloads airplane altitude angle of attack angular approximation assume atmosphere axes axis body booster C₁ calculated camber Chapter coefficient components compressor constant cruising damping derivatives differential dimensionless discussed drag dx₁ dynamic elevator engine entry equations of motion estimate Etkin flight conditions flight path flight vehicle flow fluid force formula fuel function fuselage horizontal inertial initial conditions inlet integral isentropic lift coefficient linear loading longitudinal Mach number maneuver maximum mode mode shape normal orbit parameters perturbation phugoid pitching pitching moment plane planform positive pressure problem propeller proportional propulsion quantities ramjet ratio rocket rotation Section sideslip solution specific impulse speed stability stability derivatives subsonic supersonic theory thrust trajectory transonic trim turbojet typical variable vector velocity vertical weight wing x₁)² y₁ y₁)² zero