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Supersonic flow around circular cones at angles of attack
Supersonic Flow Around Circular Cones at Angles of Attack
The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions
Preliminary Investigation of a New Type of Supersonic Inlet
The Linearized Characteristics Method and Its Application to Practical Nonlinear Supersonic Problems
The Linearized Characteristics Method and Its Application to Practical Nonlinear Supersonic Problems