A novel thrust vector nozzle with conical surface based on Coanda effect
نویسندگان
چکیده
Abstract In this paper, a novel thrust vector control method based on Coanda effect is proposed for conical surface. The of studied by computation fluid dynamic (CFD) numerical simulation. When there no side plate both sides surface, are large vortex structures nozzle wake, and the cannot be realized. After adding plate, comprehensive pitch yaw vectors was pressure ratio (NPR) 2~2.4, angles decreased with increase NPR, maximum angle 8°. And
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ژورنال
عنوان ژورنال: Journal of physics
سال: 2023
ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']
DOI: https://doi.org/10.1088/1742-6596/2472/1/012002