Z. I. Boltaev

1 ta ish

Bukhara Engineering and Technology Institute, Bukhara, Uzbekistan

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

   I. I. Safarov, A. U. Yavov, Z. I. Boltaev +2

   MaqolaAeroelasticity and Vibration ControlAIP conference proceedings20260 iqtibos

   ABIABI:AkademIndex/openalex/2026.article.006681