I am planning to do work with Supersonic nozzle design with Jet Vane Thrust Vector Control in Supersonic Fighter Aircraft. I would like to know if it is possible to implement Jet Vane TVC in Supersonic Fighter Aircrafts. Main aim is to increase in maneuverability by this work.Which Method will be suitable to perform this work Computational(CFD) or Experimental. And i need to analyse the erosion phenomena of Jet Vane . Suggest and drop your queries. Please help me to get some journal papers related to this.
Hi,
To my knowledge, TVC is already used in Russian fighter jets like Sukhoi MKIII. If you are aiming to work on the same either experimental (Which I feel will be very expensive) or CFD, proper validation is definitely required.
You can try using some CFD codes and provide the validation with some good experimental data already available or through any valid journal.
If you are using any commercial CFD codes such as ANSYS Fluent, I will be happy to help you further.
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