Application of Engineering Transition Models to an Isolated Helicopter Rotor in Hovering Flight

التفاصيل البيبلوغرافية
العنوان: Application of Engineering Transition Models to an Isolated Helicopter Rotor in Hovering Flight
المؤلفون: Ning Qin, Jason Hill, S. T. Shaw
المصدر: 43rd AIAA Aerospace Sciences Meeting and Exhibit.
بيانات النشر: American Institute of Aeronautics and Astronautics, 2005.
سنة النشر: 2005
مصطلحات موضوعية: Engineering, business.industry, law, Aerospace engineering, Helicopter rotor, business, Marine engineering, law.invention
DOI: 10.2514/6.2005-467
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::7d0994ad72cf9c2fe0d7b5dac991d236
https://doi.org/10.2514/6.2005-467
رقم الانضمام: edsair.doi...........7d0994ad72cf9c2fe0d7b5dac991d236
قاعدة البيانات: OpenAIRE