Aircraft landing gear standard model puller

2024-03-20

LAGOON is a benchmark for aircraft landing gear noise optimization. Landing gear noise is one of the important noise sources generated by aircraft during take-off and landing, which has an importan...

SMC001 Nozzle

2024-03-20

The SMC nozzle is a nozzle design adopted by NASA in spacecraft and rocket engines, which has two typical working conditions: cold jet and hot jet, and has both inflow and outflow properties, and u...

Aerodynamic characteristics of a fighter with a large angle of attack

2024-03-20

The aerodynamic performance of fighters with mounted missiles is a key focus in the design process, and in the case of large angles of attack, it faces a variety of problems such as flow diversion,...

M6 three-dimensional airfoil

2024-03-20

The M6 is a model of a wing designed by ONERA. The model underwent a series of wind tunnel tests under transonic conditions. Despite the simple geometry of the M6 wing, the transonic flow involved ...

30P30N three-section wing

2024-03-20

The 30P30N three-segment wing is a common aircraft wing design that is commonly used in high-speed aircraft, such as jets. The central segment usually has a greater thickness and strength and is us...

Simulation of the rotor blades of a rotating machinery for the whole cycle

2024-03-20

The Dimaxer solver is used to simulate a transonic rotor with 4th order precision, including steady-state, stall and other working conditions, and the transient flow characteristics such as complex...

M219 supersonic outflow field

2024-03-20

There are multiple shock waves in the M219 supersonic flow field, and the adaptive grid encryption of the shock wave position is carried out in this example, which can better capture the shock wave...

RAE2822 stabilize the shock wave

2024-03-20

Under the condition of transonic velocity, shock waves are easy to form on the upper surface of the RAE2822 airfoil, which may cause flow separation under the interaction of shock waves and turbule...

S809 blades turbulent and transitioning

2024-03-20

The S809 is a typical low-speed wind airfoil, a 21% thick laminar airfoil designed by Dan M Somers for turbines, and the low-speed experiment was completed in the low turbulence wind tunnel of the ...

NACA0012 airfoil

2024-03-20

NACA 0012 is a classic airfoil that has been extensively studied and used. In this example, the angle of attack is 15 degrees, and most of the boundary layer is turbulent in the attached surface la...

Sphere Re3700 Sphere Circulation

2024-03-20

The three-dimensional spherical flow under the subcritical Reynolds number has obvious unsteady effects, and has the characteristics of thin laminar flow boundary layer, flow separation, shear lami...

Cylinder Re200 Cylinder Flow

2024-03-20

Under this Reynolds number, there is a classic Karmen vortex street phenomenon, and the tail vortex oscillates symmetrically periodically.Comparing the results of the conformal consistency grid and...