Approximate solutions of range for constant altitude - Constant high subsonic speed flight of transport aircraft

Aerospace Science and Technology

Volumn 8, Issue 6, 2004, Pages 557-567

  Cavcar, Aydan ^a   Cavcar, Mustafa ^a  

^a ANADOLU UNIVERSITY   (Turkey)

Author keywords

Aircraft performance; Aircraft range; Optimum cruise speed; Preliminary design

Indexed keywords

APPROXIMATION THEORY; COMPRESSIBILITY; FLIGHT DYNAMICS; FUEL CONSUMPTION; PARAMETER ESTIMATION; TURBOJET ENGINES;

AIRCRAFT PERFORMANCE; AIRCRAFT RANGE; OPTIMUM CRUISE SPEED; PRELIMINARY DESIGNS;

TRANSPORT AIRCRAFT;

EID: 4243069396     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2004.04.002     Document Type: Article

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