The paper covers the numerical simulation of the gas-dynamic parameters of the nozzle passage when using an intra-nozzle ramp interceptor in order to control the thrust vector. The analysis of the resulting axial and lateral forces at various angles of interceptor deflection is carried out.
Investigation of Gas Flow Characteristics When Using Intra-Nozzle Interceptors to Control the Thrust Vector
Russ. Aeronaut.
Russian Aeronautics ; 65 , 4 ; 705-712
2022-10-01
8 pages
Article (Journal)
Electronic Resource
English
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