|
|
|
|
|
Tingkai Dai and Bo Zhang
The interaction between shock waves and turbulent boundary layers (SBLI) is a common phenomenon in transonic and supersonic aircraft wings. In this study, we simulated the SBLI of a classical NACA0012 wing at an angle of attack (AOA) of 1.4° and Mach num...
ver más
|
|
|
|
|
|
|
|
|
|
|
Tingkai Dai and Bo Zhang
Shock wave/turbulent boundary layer interaction (SBLI) is one of the most common physical phenomena in transonic wing and supersonic aircraft. In this study, the compression ramp SBLI (CR-SBLI) was simulated at a 24° corner at Mach 2.84 using the open-so...
ver más
|
|
|
|
|
|
|
|
|
|
|
Kalyani Bhide, Kiran Siddappaji and Shaaban Abdallah
The aim of this work is to highlight the significance of Fluid?Thermal?Structural Interaction (FTSI) as a diagnosis of existing designs, and as a means of preliminary investigation to ensure the feasibility of new designs before conducting experimental a...
ver más
|
|
|
|
|
|