المؤلفون: Lin Peng, Wang Dong

المصدر: Hangkong bingqi, Vol 28, Iss 4, Pp 1-6 (2021)

مصطلحات موضوعية: nozzle, aircraft and engine integration, internal and external flow, thrust vector, stealth, aircraft, aeroengine, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1631769493046-1098143134.pdf; https://doaj.org/toc/1673-5048

URL الوصول: https://doaj.org/article/f8caae89ea0647ec8b9061ef739f3a10