Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Nonlinear Aerodynamic Modeling From Flight Data Using Advanced Piloted Maneuvers and Fuzzy Logic
Measurement of the Moments and Product of Inertia of the Fairey delta 2 Aircraft
Jet-boundary corrections to a yawed model in a closed rectangular wind tunnel
Helicopter Control and Stability. Part 4 - Lateral Motion
Stability derivatives of triangular wings at supersonic speeds
Effect of product of inertia on lateral stability
Wind-Tunnel Investigation of Actuated Forebody Strakes for Yaw Control at High Angles of Attack
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model