Popov, S. A., & Gondarenko, Y. A. (2017). MATHEMATICAL MODEL OF THE MOTION OF A LIGHT ATTACK AIRCRAFT WITH EXTERNAL LOAD SLINGS IN THE EXTREME AREA OF FLIGHT MODES ACCORDING TO THE ANGLE OF ATTACK. Moscow State Technical University of Civil Aviation.
Chicago Style (17th ed.) CitationPopov, S. A., and Y. A. Gondarenko. MATHEMATICAL MODEL OF THE MOTION OF A LIGHT ATTACK AIRCRAFT WITH EXTERNAL LOAD SLINGS IN THE EXTREME AREA OF FLIGHT MODES ACCORDING TO THE ANGLE OF ATTACK. Moscow State Technical University of Civil Aviation, 2017.
MLA (9th ed.) CitationPopov, S. A., and Y. A. Gondarenko. MATHEMATICAL MODEL OF THE MOTION OF A LIGHT ATTACK AIRCRAFT WITH EXTERNAL LOAD SLINGS IN THE EXTREME AREA OF FLIGHT MODES ACCORDING TO THE ANGLE OF ATTACK. Moscow State Technical University of Civil Aviation, 2017.