This intake is the first section in which the air entering the engine passes through it. This section is a convergent or divergent duct and its task is to slow down and smooth the flow of air into the engine. If the air velocity of the inlet to the compressor is high, the velocity of air at the tip of the blades will reach the sound speed and a lot of power will flow to the compressor. If the airspeed is subsonic, this would be divergent. If the velocity is high (supersonic), this canal would be convergent. In a supersonic airflow, the air passes through a convergent duct and its velocity decreases at subsonic speeds; therefore, the entry of aircraft is divergent to reduce the speed and help the compressor.
In this analysis, it has been tried to simulate the airflow inside a jet intake using ANSYS Fluent software.
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The product which is analyzed on this page was made according to our customer’s request. The cost of this product at the first place was 1200$. This product has now been redeemed, and its cost is 349$, you can purchase it right now by clicking on “Buy Now” button in order to save your money and time.
TITLE: CFD SIMULATION OF TURBOJET INTAKE
PROJECT TYPE: AERODYNAMIC
MODULE: DENSITY BASED AND IDEAL GAS
TIME: 25 days
PRIMARY PRICE: 1200 $
PRICE IN STORE: 349$