oscar77
21st May 2014, 04:49
I'm am currently in my first year of a bachelor of Aviation course at uni. In an assignment I'm doing it require me to compile a report on an airplane (Gulfstream G300) including calculations of things such as coefficient of lift and drag etc.
Information on this plane can be hard to come by and so I have a few questions regarding figures and calculations I have used.
1. What is a realistic takeoff speed for the plane? I currently have a figure of 281 kph. Also what would be the approx landing speed?
2. Is a max cruise speed of 925 kph a realistic number because it seems way high.
3. How much bigger would the wing area be when flaps etc are extended for take-off/landing? "clean?" area is 88 m2
Any help with any of this would be greatly appreciated. Even just your best guesses would be better than my best guesses haha so I'm not worried too much about it being exact as no one is actually going to use information for anything.
Information on this plane can be hard to come by and so I have a few questions regarding figures and calculations I have used.
1. What is a realistic takeoff speed for the plane? I currently have a figure of 281 kph. Also what would be the approx landing speed?
2. Is a max cruise speed of 925 kph a realistic number because it seems way high.
3. How much bigger would the wing area be when flaps etc are extended for take-off/landing? "clean?" area is 88 m2
Any help with any of this would be greatly appreciated. Even just your best guesses would be better than my best guesses haha so I'm not worried too much about it being exact as no one is actually going to use information for anything.