Мақола

Flexural-torsional flutter of an aircraft wing with distributed parameters in subsonic flight mode

I. I. SafarovTashkent Institute of Chemical Technology, Tashkent, UzbekistanA. U. YavovBukhara Institute of Natural Resources Management of the National Research University of TIIAME, Bukhara, UzbekistanZ. I. BoltaevBukhara Engineering and Technology Institute, Bukhara, UzbekistanX. E. ErgashevBukhara Institute of Natural Resources Management of the National Research University of TIIAME, Bukhara, UzbekistanU. U. RajabovBukhara Institute of Natural Resources Management of the National Research University of TIIAME, Bukhara, Uzbekistan

AIP conference proceedingsjournal2026

ABI

Аннотация

Аннотация мавжуд эмас.

Мавзулар

Aeroelasticity and Vibration Control Heat Transfer and Mathematical Modeling Biomimetic flight and propulsion mechanisms

Идентификаторлар

DOI: 10.1063/5.0328032

Иқтибослар ва манбалар

0 та иқтибос7 та фойдаланилган манба

Кўрсаткичлар — AkademScholar