The objective with this work was to examine the effects of fitness ratio, lift over drag, lift coefficient at cruise, winglet span, wing sweep angle, wing aspect ratio, wing area and weights with respect to Mach number for a conventional business jet capable of 18 passengers. The cruise speed study range from Mach 0.88 to 0.99.
Showing posts with label (Mechanical Project) Effects of Mach Cruise Number on Conventional Civil Jet Aircraft Sizing. Show all posts
Showing posts with label (Mechanical Project) Effects of Mach Cruise Number on Conventional Civil Jet Aircraft Sizing. Show all posts
(Mechanical Project) Effects of Mach Cruise Number on Conventional Civil Jet Aircraft Sizing
The objective with this work was to examine the effects of fitness ratio, lift over drag, lift coefficient at cruise, winglet span, wing sweep angle, wing aspect ratio, wing area and weights with respect to Mach number for a conventional business jet capable of 18 passengers. The cruise speed study range from Mach 0.88 to 0.99.
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