Flight dynamics models used in different national and international projects

Aircraft Engineering and Aerospace Technology

Volumn 86, Issue 3, 2014, Pages 166-178

  Goraj, Zdobyslaw ^a  

^a WARSAW UNIVERSITY OF TECHNOLOGY   (Poland)

Author keywords

Blended wing body; Flight stability; Stability derivatives; Stability of unconventional configurations; UAV

Indexed keywords

DYNAMICS; EQUATIONS OF MOTION; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; TRANSPORT AIRCRAFT; UNMANNED AERIAL VEHICLES (UAV);

BLENDED WING BODY; BLENDED WING BODY CONFIGURATIONS; COMPUTATIONAL PROCEDURES; DESIGN/METHODOLOGY/APPROACH; FLIGHT STABILITY; INTERNATIONAL PROJECTS; PRELIMINARY DESIGN PHASE; STABILITY DERIVATIVES;

AERODYNAMIC STABILITY;

EID: 84903217289     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/AEAT-02-2013-0036     Document Type: Article

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