DJI Mavic, Air and Mini Drones
Friendly, Helpful & Knowledgeable Community
Join Us Now

Is This The Dumb Question Department?

Of course you do - don't be lazy. Actually the request is for a flight DAT file for the same aircraft and props hovering at different elevations. I have data for the M2P and MP at 10,000 ft. If you have a DAT file for (preferably) your M2P with stock props at sea level or 1500 ft that's what I need.
This one is the M2P at 478 feet. There are 3 or 4 intervals with no control inputs.
 

Attachments

  • 2019-02-14_13-35-22_FLY043.DAT
    2.5 MB · Views: 3
  • Like
Reactions: sar104
Of course you do - don't be lazy. Actually the request is for a flight DAT file for the same aircraft and props hovering at different elevations. I have data for the M2P and MP at 10,000 ft. If you have a DAT file for (preferably) your M2P with stock props at sea level or 1500 ft that's what I need.
I recall now the previous .DAT was on a very windy day. This one might be better. There were 2 hover intervals. [8 - 36] secs and [52 -89] secs.
 

Attachments

  • 2019-02-19_13-46-26_FLY045.DAT
    6.7 MB · Views: 3
Higher RPM, probably less rate of climb, more power consumption.

MP service ceiling 5000m
M2 service ceiling 6000m

The relationship is a bit more complex than that. As a highly simplified comparison, consider that both situations require the same thrust to support the aircraft. At the higher elevation, with lower air density, the props are turning faster and therefore moving the air faster. Since force is rate of change of momentum, that means that the required thrust is produced by a lower mass flux at higher speed. In other words, the product v.dm/dt is the same. But since energy goes with the mass and the square of the speed, at higher elevation, ½.v².dm/dt will be larger.
 
The relationship is a bit more complex than that. As a highly simplified comparison, consider that both situations require the same thrust to support the aircraft. At the higher elevation, with lower air density, the props are turning faster and therefore moving the air faster. Since force is rate of change of momentum, that means that the required thrust is produced by a lower mass flux at higher speed. In other words, the product v.dm/dt is the same. But since energy goes with the mass and the square of the speed, at higher elevation, ½.v².dm/dt will be larger.

Los Alamos is definitely the right city for you and Oppenheimer. Thumbswayup
 
  • Like
Reactions: sar104
The relationship is a bit more complex than that. As a highly simplified comparison, consider that both situations require the same thrust to support the aircraft. At the higher elevation, with lower air density, the props are turning faster and therefore moving the air faster. Since force is rate of change of momentum, that means that the required thrust is produced by a lower mass flux at higher speed. In other words, the product v.dm/dt is the same. But since energy goes with the mass and the square of the speed, at higher elevation, ½.v².dm/dt will be larger.
Man ... if that's the "... highly simplified comparison, ..." then I'm feeling like a monkey in a tree right now ... :D
Really interesting results guys - thanks to @sar104 and @BudWalker for getting the data together ... I'm not surprised at the increase in rpm with altitude, but I didn't think the increase in power consumption would be quite that high!
 
Last edited:
Lycus Tech Mavic Air 3 Case

DJI Drone Deals

New Threads

Forum statistics

Threads
131,416
Messages
1,562,946
Members
160,333
Latest member
ADK Dragonfly