aerodynamic chord वाक्य
उदाहरण वाक्य
मोबाइल
- Trim range is 16 33 % of mean aerodynamic chord.
- It is usually quoted as a percentage of the Mean Aerodynamic Chord.
- For all tests, the center of gravity of the model was at either 14.5 % of Mean Aerodynamic Chord ( MAC ) or 25.5 % of MAC.
- The OPTINS Namelist defines the reference parameters for the aircraft . The theoretical wing area, mean aerodynamic chord, and wing span are input along with a parameter defining the surface roughness of the aircraft.
- In aircraft analysis, static margin is defined as the distance between the center of gravity and the neutral point of the aircraft, expressed as a percentage of the mean aerodynamic chord of the wing.
- In larger aircraft, weight and balance is often expressed as a percentage of mean aerodynamic chord, or MAC . For example, assume the leading edge of the MAC is 62 inches aft of the datum.
- Staff of the Department of Civil Aviation calculated the most likely position of the centre of gravity on the fatal flight and found it was about 3.3 % of Mean Aerodynamic Chord behind the rear limit . { { # tag : ref | The position of passengers and cargo was not known precisely.
- The Chief Pilot of " Queensland Airlines " told the inquest he did not believe the accident was caused by incorrect loading of the aircraft . He said the load sheet showed the aircraft's centre of gravity was at 39.2 % of Mean Aerodynamic Chord and therefore only slightly outside the approved limit.
- If a general MAC is not given but a LeMAC ( leading edge mean aerodynamic chord ) and a TeMAC ( trailing edge mean aerodynamic chord ) are given ( both of which would be referenced as an arm measured out from the datum line ) then your MAC can be found by finding the difference between your LeMAC and your TeMAC.
- If a general MAC is not given but a LeMAC ( leading edge mean aerodynamic chord ) and a TeMAC ( trailing edge mean aerodynamic chord ) are given ( both of which would be referenced as an arm measured out from the datum line ) then your MAC can be found by finding the difference between your LeMAC and your TeMAC.
- The loaded weight of VH-BAG was determined to have been approximately but up to of fuel would have been consumed during engine running and taxying . | group = Note } } After the undercarriage retracted, the aircraft's centre of gravity was behind the rear limit by between 4.3 % and 4.9 % of Mean Aerodynamic Chord.
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